AUTHOR NAME |
PAPER TITLE |
ICAS PAPER NUMBER |
Aakkula,
J. |
DIARC PLASMA COATING FOR
RELIABLE AND DURABLE STRUCTURAL BONDING OF METALS |
ICAS2012-7.2.1 |
Abdalla, A. M. |
THE INFLUENCE OF DEMOISELLE
AIRCRAFT ON LIGHT AND GENERAL AVIATION DESIGN |
ICAS2012-1.7.ST |
Abdalla, A. M. |
AIRCRAFT EMERGENCY
EVACUATION SIMULATION USING ANT COLONY OPTIMIZATION |
ICAS2012-9.1.3 |
Abdi, F. |
COUPLED
MICROMECHANICS-FINITE ELEMENT PROGRESSIVE FAILURE DYNAMIC ANALYSIS APPROACH:
F-16 CANOPY CASE STUDY |
ICAS2012-7.7.5 |
Abdi, F. |
REAL
TIME DIAGNOSIS OF DYNAMIC FAILURE IN FUTURE AEROSPACE STRUCTURES |
ICAS2012-8.11.2 |
Abe, H. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
Abedian, A. |
EFFECT OF LATERAL PLACEMENT
OF CERAMIC AND METAL GRAINS ON THERMAL STRESS DISTRIBUTION THROUGHOUT FGMS |
ICAS2012-7.3.4 |
Abedian, A. |
FINDING TUNING FREQUENCY OF
SYMMETRIC AND ANTI-SYMMETRIC LAMB WAVES USING FEM |
ICAS2012-P3.6 |
Abedian, A. |
WAVELET-BASED ACTIVE SENSING
FOR QUANTITATIVE ASSESSMENT OF THROUGH-THICKNESS CRACK SIZE AND ANGLE IN
COMPOSITE PLATES |
ICAS2012-P3.8 |
Abedian, A. |
RISK ASSESSMENT MODELLING
FOR EVALUATING SAFETY AND IMPACT ON BUSINESS VIA A 3D RISK MATRIX |
ICAS2012-P9.2 |
Abramov, N. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
Abramov, N. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
Abu Talib, A. R. |
PERFORMANCE TEST OF A
SMALL-SCALE TURBOJET ENGINE RUNNING ON A PALM OIL BIODIESEL - JET A BLEND |
ICAS2012-4.8.1 |
Achard, P. |
APACHE : INTEGRATED HYBRID
FUEL CELL SYSTEM FOR 2-SEAT ALL ELECTRIC AIRCRAFTS PROPULSION |
ICAS2012-6.7.4 |
Adachi, K. |
INTEGRATED DESIGN METHOD OF
A ROCKET ENGINE TURBOPUMP SUB-SYSTEM FOR SUPPRESSING ROTOR LATERAL VIBRATION |
ICAS2012-4.3.4 |
Adamczak, D. |
HIFIRE-1 BOUNDARY-LAYER
TRANSITION MEASUREMENTS |
ICAS2012-3.10.3 |
Adams, N. |
AERODYNAMIC OPTIMISATION OF
A MORPHING MEMBRANE WING |
ICAS2012-3.6.3 |
Adams, N. A. |
FLOW CHARACTERISTICS OF A
HELICOPTER FUSELAGE CONFIGURATION INCLUDING A ROTATING ROTOR HEAD |
ICAS2012-2.7.3 |
Adams, N. A. |
AEROACOUSTIC ANALYSIS OF A
HELICOPTER CONFIGURATION WITH DUCTED TAIL ROTOR |
ICAS2012-3.9.1 |
Agarwal, R. K. |
ACTIVE
CONTROL OF SHOCK/BOUNDARY LAYER INTERACTION FOR TRANSONIC DRAG REDUCTION OF
AIRFOILS |
ICAS2012-2.10.4 |
Agusdinata, D. B. |
DEVELOPING OPTIMAL AIRLINE
FLEETS UNDER ENVIRONMENTAL AND CAPACITY CONSTRAINTS |
ICAS2012-7.10.1 |
Ahmad, M. T. |
PERFORMANCE TEST OF A
SMALL-SCALE TURBOJET ENGINE RUNNING ON A PALM OIL BIODIESEL - JET A BLEND |
ICAS2012-4.8.1 |
Ai, J. |
RESEARCH ON ESTIMATING
METHOD OF FUEL AND EMISSIONS USING NEURAL NETWORKS IN LTO CYCLE FOR
PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-7.11.2 |
Aksaray, D. |
STATISTICAL STABILITY AND
CONTROL ANALYSIS TO INVESTIGATE THE CONTROL EFFORT OF IMPROVING HANDLING
QUALITY CHARACTERISTICS |
ICAS2012-5.9.1 |
Alderliesten, R. C. |
ENERGY DISTRIBUTION IN GLARE
AND 2024-T3 ALUMINIUM DURING LOW-VELOCITY IMPACT |
ICAS2012-7.7.2 |
Alers, T. |
AN ASSET FOR IMPROVED
EFFICIENCY AND PUNCTUALITY IN AIR TRANSPORT |
ICAS2012-11.7.5 |
Allain, L. |
RELIABILITY ANALYSIS OF
AIRCRAFT SYSTEM ARCHITECTURES |
ICAS2012-P9.1 |
Allwood, G. |
DISTRIBUTED
OPTICAL FIBRE SMART SENSORS FOR ADVANCE SENSING SYSTEMS IN AEROSPACE VEHICLES |
ICAS2012-P6.7 |
Alonso, J. J. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
Altunlu, A. C. |
ACCELERATED LIFE CONSUMPTION
DUE TO THERMO-ACOUSTIC OSCILLATIONS IN GAS TURBINES: XFEM & CRACK |
ICAS2012-4.2.2 |
Alvarez, L. M. |
EXTRACTING DECK TREND TO
PLAN DESCENT TRAJECTORY FOR SAFE LANDING OF UAVS |
ICAS2012-11.8.3 |
Alwi, S. I. S. |
PRODUCTION
OF BIO-FUEL FROM ALGAE BIOMASS, NANNOCHLOROPSIS OCULATA, FOR ADDITION TO
KEROSENE JET A-1 |
ICAS2012-8.6.4 |
Amadori, K. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
Aminanda, Y. |
MODELLING OF IMPACT ON
SANDWICH STRUCTURE FOR FAST MAINTENANCE LOOPS |
ICAS2012-8.3.3 |
Amiryants, G. |
AEROELASTIC
MULTIDISCIPLINARY ANALYSIS OF THE FIN
WITH INNOVATIVE ADAPTIVE CONTROL |
ICAS2012-8.7.4 |
Anderson, D. |
ASSESSING
HELICOPTER SURVIVABILITY TO GROUND LAUNCHED PROJECTILES USING MULTI-FIDELITY
INVERSE SIMULATION |
ICAS2012-1.4.4 |
Anderson, D. |
DEVELOPMENT OF NAVIGATION
ALGORITHMS FOR NAP-OF-THE-EARTH UAV FLIGHT IN A CONSTRAINED URBAN ENVIRONMENT |
ICAS2012-11.9.1 |
Andreeva-Mori, A. |
A STUDY ON FINDING A
SUBSTITUTE TO THE FIRST COME- FIRST SERVED RULE APPLIED TO AIRCRAFT
SEQUENCING |
ICAS2012-10.8.2 |
Anemaat, W. A. J. |
DESIGN METHODS FOR AN
UNCONVENTIONAL SPLIT WING AIRCRAFT CONFIGURATION |
ICAS2012-1.3.1 |
Anghileri, M. |
EXPERIMENTAL AND NUMERICAL
ASSESSMENT OF HELICOPTER SUBFLOOR CRASHWORTHINESS |
ICAS2012-8.1.1 |
Anghileri, M. |
PRELIMINARY INVESTIGATION ON
THE FEASIBILITY OF A BIRD SURROGATE FOR FULL-SCALE BIRD IMPACT TEST |
ICAS2012-8.3.1 |
Anton, E. |
AN INTERDISCIPLINARY
APPROACH FOR A VIRTUAL AIR-TRAFFIC SYSTEM SIMULATION FOR SUBJECTIVE
ASSESSMENT IN VR ENVIRONMENTS |
ICAS2012-7.10.3 |
Antunes, A. P. |
ON THE EFFECTS OF TURBULENCE
MODELING AND GRID REFINEMENT ON HIGH-LIFT CONFIGURATION AERODYNAMIC
SIMULATIONS |
ICAS2012-2.3.1 |
Aoki, Y. |
EVALUATION ON DISCRETE
SOURCE DAMAGES OF CFRP STIFFENED PANELS |
ICAS2012-7.7.1 |
Aoyama, S. |
DEVELOPMENT OF MOBILE
PASSIVE SECONDARY SURVEILLANCE RADAR |
ICAS2012-P8.8 |
Aoyama, T. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
Appel, B. |
UAS DESIGN REQUIREMENTS FOR
OPERATION IN COLOMBIAN MOUNTAIN ENVIRONMENTS |
ICAS2012-1.8.ST |
Arai, N. |
COMPARISON OF PERFORMANCE OF
PROPELLER BLADES BY DIFFERENCE IN PLANAR SHAPE |
ICAS2012-4.6.ST1 |
Archambaud, J. -P. |
STABILITY ANALYSIS ON
NATURAL LAMINAR FLOW WING IN SUPERSONIC FLOW: ONERA-JAXA JOINT RESEARCH
PROGRAM |
ICAS2012-3.10.1 |
Arevalo, J. L. L. |
WEIGHT ON WHEEL SYSTEM BASED
ON STRAIN GAUGES |
ICAS2012-6.11.2 |
Arimoto, M. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
Arnal, D. |
STABILITY ANALYSIS ON
NATURAL LAMINAR FLOW WING IN SUPERSONIC FLOW: ONERA-JAXA JOINT RESEARCH
PROGRAM |
ICAS2012-3.10.1 |
Arnaldo, R. |
HALA!: TOWARDS HIGHER LEVELS
OF AUTOMATION IN ATM. POSITION PAPER -STATE OF THE ART AND RESEARCH AGENDA |
ICAS2012-10.1.1 |
Arnaldo, R. |
AIRCRAFT FLIGHT TRAJECTORY
DEVIATION IN THE STANDARD INSTRUMENT DEPARTURES. OPERATORS PENALTIES |
ICAS2012-10.10.2 |
Arnaldo, R. |
LEGAL AND TECHNICAL
IMPLICATIONS OF THE SAFETY RECOMMENDATIONS ISSUED IN THE FINAL REPORTS OF THE
CIVIL AIR ACCIDENTS AND INCIDENTS INVESTIGATIONS |
ICAS2012-9.4.ST |
Asai, K. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
Aso, S. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
Atencio, B. N. |
MEASUREMENTS AND PREDICTION
OF LAMINAR-TURBULENT TRANSITION AT HIGH FREE-STREAM TURBULENCE & PRESSURE
GRADIENTS |
ICAS2012-3.10.5 |
Atinault, O. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
Atkin, C. J. |
RECENT DEVELOPMENTS TO THE
VISCOUS GARABEDIAN AND KORN METHOD |
ICAS2012-2.11.3 |
Atobe, T. |
STABILIZING EFFECT OF
LONGITUDINAL-WALL OSCILLATION ON 2D CHANNEL FLOW |
ICAS2012-P2.12 |
Attia, M. |
PRE-STRESSED MODAL ANALYSIS
OF A TURBINE SPACER |
ICAS2012-P4.11 |
Aubert, S. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
Aubert, S. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
Aubry, S. |
MODELLING AIR TRAFFIC IMPACT
ON LOCAL AIR QUALITY WITH IESTA AND ADMS-AIRPORT: VALIDATION USING FIELD
MEASUREMENTS ON A REGIONAL AIRPORT |
ICAS2012-4.9.4 |
Avakyan, A. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
Azevedo, J. L. F. |
ON THE EFFECTS OF TURBULENCE
MODELING AND GRID REFINEMENT ON HIGH-LIFT CONFIGURATION AERODYNAMIC
SIMULATIONS |
ICAS2012-2.3.1 |
Bae, J. C. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
Baena, S. |
COLD FUEL TEST RIG TO
INVESTIGATE ICE ACCRETION ON DIFFERENT PUMP INLET FILTER-MESH SCREENS |
ICAS2012-6.5.2 |
Bagassi, S. |
DESIGN ANALYSIS FOR HYBRID
PROPULSION |
ICAS2012-6.7.5 |
Bagassi, S. |
INNOVATION IN MAN MACHINE
INTERFACES: USE OF 3D CONFORMAL SYMBOLS IN THE DESIGN OF FUTURE HUDS (HEAD UP
DISPLAYS) |
ICAS2012-9.7.2 |
Bagassi, S. |
A
META-HEURISTIC APPROACH TO SIMULATE TAXI OPERATIONS |
ICAS2012-P8.7 |
Bagg, R. L. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
Bai, J. |
APPLICATION
OF TWO TRANSITION MODELS TO FLOWS AROUND AIRFOILS |
ICAS2012-2.4.4 |
Bain, M. |
ENGINE-OUT TAKEOFF PATH
OPTIMIZATION OUT OF TERRAIN CHALLENGING AIRPORTS |
ICAS2012-5.8.2 |
Bakar, A. |
MULTIDISCIPLINARY EVALUATION
OF TRUSS-BRACED WING FOR FUTURE GREEN AIRCRAFT |
ICAS2012-1.10.ST |
Baker, J. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
Baker, J. W. C. |
DEVELOPING THE USE OF
NEURAL-NETWORK TEST TECHNOLOGY FROM AVIONICS TO WIRING SYSTEMS |
ICAS2012-12.5.1 |
Bakker, G. J. |
ANALYZING SEPARATION LOSS
EVENTS IN TWO-PAIRED AIRCRAFT TRAILING CONDUCTING AIRBORNE TIME SPACING BASED
CONTINUOUS DESCENT ARRIVAL |
ICAS2012-10.8.3 |
Balbo, M. |
TURBOJET ANALYTICAL MODEL
DEVELOPMENT AND VALIDATION |
ICAS2012-4.10.5 |
Barber, T. J. |
PROGRESS IN UNDERSTANDING
TRANSONIC AND SUPERSONIC GROUND EFFECT AERODYNAMICS |
ICAS2012-10.6.3 |
Baron, W. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
Barriere, L. |
POSTBUCKLING COMPUTATION OF
LARGE STIFFENED STRUCTURES |
ICAS2012-8.1.3 |
Barter, S. A. |
INVESTIGATION OF AN
IN-SERVICE CRACK SUBJECTED TO AERODYNAMIC BUFFET AND MANOEUVRE LOADS AND
EXPOSED TO AN CORROSIVE ENVIRONMENT |
ICAS2012-7.9.1 |
Barth, J. E. |
STREAMWISE PORTHOLE FUEL
INJECTION FOR BOUNDARY-LAYER COMBUSTION INSIDE A SCRAMJET ENGINE |
ICAS 2012-P4.16 |
Barthmes, S. |
NUMERICAL INVESTIGATION OF
THE EFFECT OF INFLOW DISTORTIONS ON TRANSONIC AXIAL COMPRESSOR STAGES WITH 2D
AND 3D CALCULATIONS |
ICAS2012-4.6.2 |
Bartsch, M. |
NUMERICAL SIMULATIONS AND
EXPERIMENTAL INVESTIGATIONS ON QUASI-STATIC AND CYCLIC MIXED MODE
DELAMINATION OF MULTIDIRECTIONAL CFRP LAMINATES |
ICAS2012-7.4.2 |
Basaglia, M. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
Basov, V. N. |
FATIGUE DESIGN PROCEDURE OF
LONGITUDINAL AND TRANSVERSE FUSELAGE JOINTS |
ICAS2012-12.4.2 |
Basset, P. -M. |
MODELING OF LOSS OF TAIL
ROTOR EFFECTIVENESS CONDUCTING TO UNANTICIPATED YAW |
ICAS2012-5.10.3 |
Batten, D. |
ALTERNATIVE AVIATION FUEL
FEEDSTOCK: THE MICROALGAE SOLUTION? |
ICAS2012-8.6.2 |
Baxley, B. T. |
INTERVAL MANAGEMENT WITH
SPACING TO PARALLEL DEPENDENT RUNWAYS (IMSPIDR) EXPERIMENT AND RESULTS |
ICAS2012-9.10.3 |
Bayandor, J. |
DETAILED POST-SOFT IMPACT
PROGRESSIVE DAMAGE ANALYSIS FOR A HYBRID STRUCTURE JET ENGINE |
ICAS2012-4.2.3 |
Bayandor, J. |
COUPLED
MICROMECHANICS-FINITE ELEMENT PROGRESSIVE FAILURE DYNAMIC ANALYSIS APPROACH:
F-16 CANOPY CASE STUDY |
ICAS2012-7.7.5 |
Bayandor, J. |
REAL
TIME DIAGNOSIS OF DYNAMIC FAILURE IN FUTURE AEROSPACE STRUCTURES |
ICAS2012-8.11.2 |
Bayandor, J. |
A
LEAP IN LEARNED BIO-INSPIRED FLIGHT |
ICAS2012-9.5.ST |
Beaumier, P. |
NUMERICAL TOOLS DEVELOPED AT
ONERA FOR THE AERODYNAMIC ASSESSMENT OF PROPELLERS AND COUNTER-ROTATING OPEN
ROTORS |
ICAS2012-4.7.1 |
Becker, R. -G. |
IMPACT OF ALTERNATIVE FUELS
ON ENGINE PERFORMANCE AND CO2-EMISSIONS |
ICAS2012-8.6.3 |
Beguin, B. |
AERODYNAMIC OPTIMISATION OF
A MORPHING MEMBRANE WING |
ICAS2012-3.6.3 |
Belo, E. M. |
AIRCRAFT EMERGENCY
EVACUATION SIMULATION USING ANT COLONY OPTIMIZATION |
ICAS2012-9.1.3 |
Bendfeldt, P. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
Benedictus, R. |
ENERGY DISTRIBUTION IN GLARE
AND 2024-T3 ALUMINIUM DURING LOW-VELOCITY IMPACT |
ICAS2012-7.7.2 |
Berge, M. E. |
THE GENERALIZED ARRIVAL
PLANNER (GARP): MODELING AND ANALYSIS FOR ARRIVAL PLANNING |
ICAS2012-10.9.3 |
Bergman, M. |
MORE ELECTRICAL
ENVIRONMENTAL CONTROL SYSTEM SIMULATION |
ICAS2012-6.6.4 |
Berlowitz, I. |
CARGO FIRE PROTECTION
SYSTEMS FOR FREIGHTER CONVERSIONS |
ICAS2012-6.10.1 |
Berry, P. |
RECYCLING OLD WEIGHT
ASSESSMENT METHODS AND GIVING THEM NEW LIFE IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS2012-1.1.2 |
Berry, P. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
Bertini, G. |
DESIGN ANALYSIS FOR HYBRID
PROPULSION |
ICAS2012-6.7.5 |
Bertsch, L. |
FLIGHT TESTING OF NOISE
ABATING RNP PROCEDURES AND STEEP APPROACHES |
ICAS2012-4.9.1 |
Bespalov, V. A. |
COMPUTATIONAL AND
EXPERIMENTAL RESEARCH OF BOLT JOINTS OF METAL AND COMPOSITE IN AIRFRAMES |
ICAS2012-8.4.ST |
Bibel, G. |
BEYOND
THE BLACK BOX: THE FORENSICS OF AIRPLANE CRASHES |
ICAS2012-0.2 |
Bil, C. |
METHODOLOGY FOR A
PRELIMINARY DESIGN STUDY OF A BOX-WING AIRLINER |
ICAS2012-1.10.3 |
Bil, C. |
IMPROVEMENTS FOR OPTIMUM
PROFILE SCHEDULING OF USER PREFERRED TRAJECTORIES |
ICAS2012-10.3.2 |
Blom, H. |
ANALYZING SEPARATION LOSS
EVENTS IN TWO-PAIRED AIRCRAFT TRAILING CONDUCTING AIRBORNE TIME SPACING BASED
CONTINUOUS DESCENT ARRIVAL |
ICAS2012-10.8.3 |
Blondeau, C. |
AIRCRAFT CONCEPTUAL DESIGN
IN A MULTI-LEVEL, MULTI-FIDELITY, MULTI-DISCIPLINARY OPTIMIZATION PROCESS |
ICAS2012-1.6.4 |
Blumrich, F. |
PARAMETRIC STUDY OF RAIM
PERFORMANCE USING NEARLY UNIFORMLY DISTRIBUTED REFERENCE POINTS ON THE
EARTH’S SURFACE |
ICAS2012-6.9.4 |
Boblak, I. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
Bock, M. |
IMPROVING THE PRODUCTION
QUALITY OF THE ADVANCED AUTOMATED FIBER PLACEMENT PROCESS BY MEANS OF ONLINE
PATH CORRECTION |
ICAS2012-6.1.3 |
Böck, P. M. |
AIRPORT CAPACITY
REPRESENTATION BASED ON AIRSIDE SIMULATIONS |
ICAS2012-10.10.1 |
Boehnke, D. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
Böhnke, D. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
Bojovschi, A. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
Bolinches i-Gisbert, M. |
MODELLING OF A WARPING WING
FOR ENERGY CONSUMPTION MINIMIZATION |
ICAS2012-1.3.4 |
Bolsunovsky, A. L. |
AN EXPERIENCE IN AERODYNAMIC
DESIGN OF TRANSPORT AIRCRAFT |
ICAS2012-2.9.3 |
Bombardier, Y. |
PROBABILISTIC RISK ANALYSIS
FOR AIRCRAFT STRUCTURES WITH LIMITED IN-SERVICE DAMAGES |
ICAS2012-7.9.3 |
Bondarenko, D. |
EXPERIMENTAL INVESTIGATIONS
OF HYDRAULIC DEVICES PERFORMANCE IN AVIATION ENGINE COMPARTMENT |
ICAS2012-P2.10 |
Borello, F. |
VERY-LONG ENDURANCE SOLAR
POWERED AUTONOMOUS UAVS: ROLE AND CONSTRAINTS FOR GMES APPLICATIONS |
ICAS2012-4.7.5 |
Borello, F. |
MORE/ALL ELECTRIC AIRCRAFT
BASED ON FUEL CELL ENERGY SYSTEM: THE ENFICA-FC EXPERIENCE |
ICAS2012-6.7.2 |
Borovoy, V. |
NUMERICAL SIMULATION OF
THREE-DIMENSIONAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTION ON SHARP AND BLUNTED
FLAT PLATE |
ICAS2012-2.4.2 |
Bortholin, T. |
COMPUTATIONAL INVESTIGATION
OF ICING CONTAMINATION ON AIRFOIL |
ICAS2012-P2.19 |
Bos, T. |
IMPLEMENTING TIME BASED CDA
OPERATIONS IN A MEDIUM-HIGH DENSITY ATM ENVIRONMENT |
ICAS2012-10.8.1 |
Bosbach, J. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
Bosnyakov, S. M. |
AN EXPERIENCE OF USING
NUMERICAL METHODS IN EXPERIMENTAL INVESTIGATIONS OF TsAGI |
ICAS2012-P2.6 |
Bowcutt, K. |
HIFIRE: AN INTERNATIONAL COLLABORATION TO ADVANCE THE SCIENCE AND TECHNOLOGY OF HYPERSONIC FLIGHT |
ICAS2012-0.8 |
Bowcutt, K. |
REAL
TIME DIAGNOSIS OF DYNAMIC FAILURE IN FUTURE AEROSPACE STRUCTURES |
ICAS2012-8.11.2 |
Boyce, R. |
ROBUST DESIGN OPTIMIZATION
OF HIGH-PERFORMANCE AXISYMMETRIC SCRAMJETS BASED ON SURROGATE-ASSISTED
EVOLUTIONARY ALGORITHMS |
ICAS2012-4.11.3 |
Boyce, R. B. |
NUMERICAL MODELLING OF
POROUS FUEL INJECTION IN A RADICAL FARMING SCRAMJET |
ICAS2012-4.11.1 |
Boyce, R. B. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
Boyce, R. R. |
THERMAL NON-EQUILIBRIUM
EFFECTS IN RADICAL FARMING SCRAMJETS |
ICAS2012-11.4.1 |
Boykett, R. |
AGEING AIRCRAFT SYSTEMS
& COST EFFECTIVE SAFETY |
ICAS2012-12.3.2 |
Boykett, R. |
QUANTITATIVE FRACTOGRAPHY
MARKERS FOR DETERMINING FATIGUE CRACK GROWTH RATES IN ALUMINIUM AND TITANIUM
AIRCRAFT STRUCTURES |
ICAS2012-12.4.1 |
Bragin, A. A. |
DEVELOPMENT OF THE AUTOMATED
SYSTEM ON THE BASIS OF NEURAL NETWORKS FOR FLIGHT SAFETY OF AIRCRAFT |
ICAS2012-5.2.2 |
Brandt, M. |
MICROSTRUCTURE AND
MECHANICAL PROPERTIES OF LASER CLADDING REPAIR OF AISI 4340 STEEL |
ICAS2012-12.4.4 |
Braun, R. |
AIRCRAFT SYSTEM SIMULATION
FOR PRELIMINARY DESIGN |
ICAS2012-1.9.3 |
Breitsamter, C. |
FLOW CHARACTERISTICS OF A
HELICOPTER FUSELAGE CONFIGURATION INCLUDING A ROTATING ROTOR HEAD |
ICAS2012-2.7.3 |
Breitsamter, C. |
AERODYNAMIC OPTIMISATION OF
A MORPHING MEMBRANE WING |
ICAS2012-3.6.3 |
Breitsamter, C. |
VORTEX FLOW MANIPULATION ON
GENERIC DELTA WING CONFIGURATIONS |
ICAS2012-3.6.4 |
Breitsamter, C. |
AEROACOUSTIC ANALYSIS OF A
HELICOPTER CONFIGURATION WITH DUCTED TAIL ROTOR |
ICAS2012-3.9.1 |
Brett, M. |
APPLICATION OF THE RANGE
SAFETY TEMPLATE TOOLKIT TO UAS RISK HAZARD ANALYSES SUPPORTING AIRWORTHINESS
REGULATION |
ICAS2012-9.2.3 |
Brezillon, J. |
A FULLY AUTOMATED CAD-BASED
FRAMEWORK FOR SHAPE OPTIMIZATION |
ICAS2012-11.10.1 |
Brezillon, J. |
NUMERICAL STUDY OF THE
REYNOLDS NUMBER EFFECT ON LOW ASPECT
RATIO WINGS AT LOW SPEED |
ICAS2012-2.10.2 |
Briceno, S. I. |
A COMPETITIVE AND
REAL-OPTIONS FRAMEWORK FOR THE ECONOMIC ANALYSIS OF LARGE AEROSPACE PROGRAMS |
ICAS2012-6.3.2 |
Brieschenk, S. |
NUMERICAL MODELLING OF
POROUS FUEL INJECTION IN A RADICAL FARMING SCRAMJET |
ICAS2012-4.11.1 |
Brieschenk, S. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
Brisbane Team, DSTO AVD |
HIFIRE-1 BOUNDARY-LAYER
TRANSITION MEASUREMENTS |
ICAS2012-3.10.3 |
Brooks, L. A. |
EXPERIMENTAL INVESTIGATION
OF FLAT PLATE SELF-NOISE REDUCTION USING TRAILING EDGE SERRATIONS |
ICAS2012-9.11.1 |
Brouwers, Y. H. A. |
THE DESIGN AND ENGINEERING
ENGINE. TOWARDS A MODULAR SYSTEM FOR COLLABORATIVE AIRCRAFT DESIGN |
ICAS2012-6.3.3 |
Brown, L. J. |
EMERGING WIRELESS
TECHNOLOGIES TO IMPROVE AIRBORNE AVIATION SECURITY |
ICAS2012-9.6.2 |
Brunello, D. |
NUMERICAL AND EXPERIMENTAL
ANALYSIS OF A REPRESENTATIVE ADF HELICOPTER FUSELAGE |
ICAS2012-2.7.2 |
Brunet, M. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
Brunner, D. |
LAY-UP OPTIMIZATION OF
COMPOSITE PLATES TO DELAY MODE-JUMP INSTABILITIES |
ICAS2012-7.1.ST |
Bueker, K. |
AN ASSET FOR IMPROVED
EFFICIENCY AND PUNCTUALITY IN AIR TRANSPORT |
ICAS2012-11.7.5 |
Buisson, M. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
Bukov, V. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
Buzoverya, N. P. |
AN EXPERIENCE IN AERODYNAMIC
DESIGN OF TRANSPORT AIRCRAFT |
ICAS2012-2.9.3 |
Buzuluk, V. I. |
ADVANCED AEROSPACE SYSTEMS
WITH INTERCONTINENTAL AND GLOBAL RANGE OF FLIGHT |
ICAS2012-1.5.2 |
Cabut, A. |
FAULT DETECTION AND
RECONFIGURATION APPLIED TO A HELICOPTER SWASHPLATE ACTUATOR |
ICAS2012-5.1.2 |
Cai, Y. |
THE PERFORMANCE COMPUTATION
OF THE HOT AIR ANTI-ICING SYSTEM OF AN AERO-ENGINE CONE |
ICAS2012-2.6.2 |
Cairns, K. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
Callantine, T. |
RESOLVING OFF-NOMINAL
SITUATIONS IN SCHEDULE-BASED TERMINAL AREA OPERATIONS: RESULTS FROM A
HUMAN-IN-THE-LOOP SIMULATION |
ICAS2012-10.5.2 |
Callus, P. J. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
Cambier, L. |
THE ONERA ELSA CFD SOFTWARE
: INPUT FROM RESEARCH AND FEEDBACK FROM INDUSTRY |
ICAS2012-2.1.1 |
Campbell, D. |
A CAPABILITY FRAMEWORK FOR
MULTIPLE HETEROGENEOUS UAVS: FROM A MISSION COMMANDER'S PERSPECTIVE |
ICAS2012-9.7.3 |
Campbell, D. A. |
THE AFFECT OF SCREEN SIZE ON
MISSION COMMANDER’S SITUATION AWARENESS |
ICAS2012-9.7.5 |
Campos, L. M. B. C. |
A PROBABILITY ASSESSMENT OF
THE FLIGHT SAFETY RELEVANT TO COLLISION AVOIDANCE |
ICAS2012-10.7.5 |
Campos, L. M. B. C. |
ON SOUND GENERATION BY
MOVING SURFACES AND CONVECTED SOURCES IN A FLOW |
ICAS2012-P2.8 |
Campos, L. M. B. C. |
ANALYTICAL NATURAL
FREQUENCIES OF TAPERED WINGS |
ICAS2012-P3.2 |
Canamar, A. |
ADVANCE SEAPLANE CONCEPTUAL
DESIGN ADAPTING TRIMARAN BOAT HULL CONCEPT |
ICAS2012-2.1.3 |
Cao, X. |
A NEW APPROACH FOR RE-ENTRY
VEHICLE TRAJECTORY PLANNING AND GUIDANCE |
ICAS2012-5.7.5 |
Cao, X. |
MANEUVERING TARGET TRACKING
BASED ON THE EKF |
ICAS2012-P5.2 |
Capararo, D. |
FINITE ELEMENT SIMULATION OF
CRACK PROPAGATION IN MILITARY AIRCRAFT COATINGS |
ICAS2012-7.2.3 |
Capra, B. R. |
NUMERICAL MODELLING OF
POROUS FUEL INJECTION IN A RADICAL FARMING SCRAMJET |
ICAS2012-4.11.1 |
Capron, W. R. |
INTERVAL MANAGEMENT WITH
SPACING TO PARALLEL DEPENDENT RUNWAYS (IMSPIDR) EXPERIMENT AND RESULTS |
ICAS2012-9.10.3 |
Carr, T. |
A NON-WEIGHT BASED,
MANUFACTURING INFLUENCED DESIGN (MIND) METHODOLOGY FOR PRELIMINARY DESIGN |
ICAS2012-6.4.3 |
Carrier, G. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
Carrier, G. |
AIRCRAFT CONCEPTUAL DESIGN
IN A MULTI-LEVEL, MULTI-FIDELITY, MULTI-DISCIPLINARY OPTIMIZATION PROCESS |
ICAS2012-1.6.4 |
Carrier, G. |
AUTOMATED CHAIN FOR
AERODYNAMIC COMPUTATIONS MEETING AIRCRAFT TRIMMING REQUIREMENTS |
ICAS2012-2.10.1 |
Castanie, B. |
POSTBUCKLING COMPUTATION OF
LARGE STIFFENED STRUCTURES |
ICAS2012-8.1.3 |
Castanié, B. |
MODELLING OF IMPACT ON
SANDWICH STRUCTURE FOR FAST MAINTENANCE LOOPS |
ICAS2012-8.3.3 |
Castelletti, L.-M. L. |
PRELIMINARY INVESTIGATION ON
THE FEASIBILITY OF A BIRD SURROGATE FOR FULL-SCALE BIRD IMPACT TEST |
ICAS2012-8.3.1 |
Castillon, L. |
EVALUATION OF A MULTIPLE
FREQUENCY PHASE LAGGED METHOD FOR UNSTEADY NUMERICAL SIMULATIONS OF
MULTISTAGE TURBOMACHINERY |
ICAS2012-4.3.1 |
Catalano, F. M. |
THE INFLUENCE OF DEMOISELLE
AIRCRAFT ON LIGHT AND GENERAL AVIATION DESIGN |
ICAS2012-1.7.ST |
Catalano, F. M. |
AIRFOIL SELF NOISE REDUCTION
BY APPLICATION OF DIFFERENT TYPES OF TRAILING EDGE SERRATIONS |
ICAS2012-3.11.1 |
Catalano, F. M. |
TRAILING EDGE TREATMENT TO
ENHANCE HIGH LIFT SYSTEM PERFORMANCE |
ICAS2012-3.2.3 |
Catalano, F. M. |
WIND TUNNEL TESTING OF
POROUS DEVICES FOR THE REDUCTION OF FLAP SIDE-EDGE NOISE |
ICAS2012-9.11.2 |
Catalano, F. M. |
COMPUTATIONAL INVESTIGATION
OF ICING CONTAMINATION ON AIRFOIL |
ICAS2012-P2.19 |
Cattan, E. |
AEROELASTIC SIMULATION OF
FLEXIBLE FLAPPING WING BASED ON STRUCTURAL FEM AND QUASI-STEADY AERODYNAMIC
MODEL |
ICAS2012-8.5.1 |
Cattaneo, G. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
Cavagna, L. |
NEOCASS: AN OPEN SOURCE
ENVIRONMENT FOR THE AEROELASTIC ANALYSIS AT CONCEPTUAL DESIGN LEVEL |
ICAS2012-8.10.1 |
Cazzato, L. |
PRELIMINARY DESIGN OF A
FUEL-CELL-BASED HYBRID-ELECTRICAL UAV |
ICAS2012-1.8.2 |
Cecrdle, J. |
EIGENVALUE AND FLUTTER
SENSITIVITY ANALYSIS OF AIRLINER WING |
ICAS2012-P3.1 |
Ceisel, J. |
A NON-WEIGHT BASED,
MANUFACTURING INFLUENCED DESIGN (MIND) METHODOLOGY FOR PRELIMINARY DESIGN |
ICAS2012-6.4.3 |
Ceisel, J. |
A METHODOLOGY FOR PARAMETRIC
PRODUCTION PLANNING IN PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-6.4.4 |
Celikovsky, S. |
STABILIZATION OF
LONGITUDINAL AIRCRAFT MOTION USING MODEL PREDICTIVE CONTROL AND EXACT
LINEARIZATION |
ICAS2012-P5.11 |
Ceron, E. D. |
TRAILING EDGE TREATMENT TO
ENHANCE HIGH LIFT SYSTEM PERFORMANCE |
ICAS2012-3.2.3 |
Cervinka, J. |
WIND TUNNEL AND CFD STUDY OF
AIRFOIL WITH AIRBRAKE |
ICAS2012-10.6.ST1 |
Cestino, E. |
VERY-LONG ENDURANCE SOLAR
POWERED AUTONOMOUS UAVS: ROLE AND CONSTRAINTS FOR GMES APPLICATIONS |
ICAS2012-4.7.5 |
Cestino, E. |
MORE/ALL ELECTRIC AIRCRAFT
BASED ON FUEL CELL ENERGY SYSTEM: THE ENFICA-FC EXPERIENCE |
ICAS2012-6.7.2 |
Chaboud, T. |
AUTOMATED CONFLICT-FREE
PLANNING: EXPERIMENTS ON REAL AIR TRAFFIC DATA |
ICAS2012-10.1.2 |
Chaboud, T. |
MODELLING AIR TRAFFIC IMPACT
ON LOCAL AIR QUALITY WITH IESTA AND ADMS-AIRPORT: VALIDATION USING FIELD
MEASUREMENTS ON A REGIONAL AIRPORT |
ICAS2012-4.9.4 |
Chai, J. |
TRANSONIC
DRAG REDUCTION ON A SUPERCRITICAL WING SECTION USING SHOCK CONTROL BUMPS |
ICAS2012-P2.3 |
Chaitanya, M. V. R. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
Chamberlain, J. |
CONCEPT OF INTEGRATION FOR
UAS OPERATIONS IN THE NAS |
ICAS2012-10.7.1 |
Chandrasekhara, M. |
WATER TUNNEL FORCE AND
MOMENT STUDIES OF A MANEUVERING UCAV 1303 AND THEIR CONTROL |
ICAS2012-3.1.3 |
Chang, C. W. T. |
EXPERIMENTAL INVESTIGATION
OF A BI-PLANE MICRO AIR VEHICLE |
ICAS2012-3.3.4 |
Changenet, C. |
COUPLING MECH. & THERMAL
MODELS IN PRELIMINARY DESIGN OF POWER TRANSMISSIONS DRIVEN BY THERMAL ISSUES |
ICAS2012-6.6.1 |
Chapelle, L. |
ASSESSMENT OF STRUCTURAL
EFFECT OF SELECTIVE STITCHING ON COMPOSITE SKIN-STIFFENER BONDING |
ICAS2012-8.9.1 |
Chaplygin, V. |
COMPUTATIONAL AND
EXPERIMENTAL RESEARCH OF BOLT JOINTS OF METAL AND COMPOSITE IN AIRFRAMES |
ICAS2012-8.4.ST |
Chassaing, J. -C. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
Chassaing, P. |
MODELING OF THE INTERACTION
BETWEEN A TURBULENT FLOW AND AN ABLATABLE MATERIAL |
ICAS2012-3.8.2 |
Che Idris, A. |
PERFORMANCE ANALYSIS OF A
SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
ICAS2012-P4.12 |
Che, B. |
IMPROVED EXACT STRIP
POSTBUCKLING ANALYSIS FOR ANISOTROPIC PLATES WITH FIXED, FREE AND STRAIGHT
EDGES |
ICAS2012-8.2.1 |
Che, H. |
TRANSONIC
DRAG REDUCTION ON A SUPERCRITICAL WING SECTION USING SHOCK CONTROL BUMPS |
ICAS2012-P2.3 |
Chedrik, V. |
ANALYSIS OF STATIC AND
DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW |
ICAS2012-8.10.4 |
Chen, H. X. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
Chen, J. |
RESEARCH ON AIRBORNE
INTELLIGENT HYDRAULIC PUMP SYSTEM |
ICAS2012-6.10.3 |
Chen, N. |
UNCERTAINTY QUANTIFICATION
IN THE DEVELOPMENT OF AVIATION OPERATIONS TO REDUCE AVIATION EMISSIONS AND
CONTRAILS |
ICAS2012-7.10.2 |
Chen, T. |
A CAPABILITY FRAMEWORK FOR
MULTIPLE HETEROGENEOUS UAVS: FROM A MISSION COMMANDER'S PERSPECTIVE |
ICAS2012-9.7.3 |
Chen, T. |
PATH PLANNING FOR MULTI
HELICOPTER COORDINATED RESCUE |
ICAS2012-P8.5 |
Chen, X. |
CONTROL ALLOCATION FOR
AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS DURING TAKEOFF AND LANDING PHASES |
ICAS2012-5.3.3 |
Chen, Y. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
Chen, Y. |
RESEARCH FOR JET FLOW INFLUENCES TO WING-MOUNTED CIVIL
AIRCRAFT AERODYNAMIC CHARACTERISTICS |
ICAS2012-2.9.1 |
Chen, Z. |
NUMERICAL
SIMULATION OF BIRD-STRIKING PROCESS AND ITS EXPERIMENTAL VERIFICATION |
ICAS2012-8.9.4 |
Cheng, H. |
INFORMATION THEORY APPLIED
TO A SELF-ORGANISED, UNMANNED AERIAL SYSTEM |
ICAS2012-11.7.4 |
Cheng, J. -H. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
Chernoray, V. |
MEASUREMENTS AND PREDICTION
OF LAMINAR-TURBULENT TRANSITION AT HIGH FREE-STREAM TURBULENCE & PRESSURE
GRADIENTS |
ICAS2012-3.10.5 |
Chernov, A. V. |
STRENGTH CRITERIA
DEVELOPMENT FOR COMPOSITE STRUCTURES BASING ON SOLUTIONS SUPERPOSITION FOR
MODELS OF DIFFERENT LEVELS |
ICAS2012-7.1.2 |
Chernov, A. V. |
INVESTIGATION OF CRACK
PROPAGATION BY OPTICAL INTERFEROMETRIC MEASUREMENTS OF LOCAL DEFORMATION
RESPONSE |
ICAS2012-7.9.2 |
Chernyshov, V. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
Chevagin, A. |
INTAKE CAPABILITY
IMPROVEMENTS IN RAMJET-TYPE PROPULSION SYSTEM |
ICAS2012-P4.3 |
Chiesa, S. |
TURBOJET ANALYTICAL MODEL
DEVELOPMENT AND VALIDATION |
ICAS2012-4.10.5 |
Chircop, K. |
A PROPOSAL FOR REVISED
APPROACHES AND PROCEDURES TO MALTA INTERNATIONAL AIRPORT |
ICAS2012-4.9.3 |
Chircop, K. |
BI-OBJECTIVE PSEUDOSPECTRAL
OPTIMAL CONTROL TECHNIQUES FOR AIRCRAFT TRAJECTORY OPTIMIZATION |
ICAS2012-P5.6 |
Cho, H. H. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
Choi, B. |
EFFECT OF VENT MIXER TO
MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
ICAS2012-P4.4 |
Choi, H. |
VISION-BASED UAV GUIDANCE
AND ESTIMATION FOR AERIAL TARGET TRACKING |
ICAS2012-11.3.2 |
Choi, H. -L. |
A PEG-BASED ASCENDING
GUIDANCE ALGORITHM FOR RAMJET-POWERED VEHICLES |
ICAS2012-5.7.4 |
Christensen, S. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
Chung, T. H. |
EXTENDING AUTONOMY
CAPABILITIES FOR UNMANNED SYSTEMS WITH CRUSER |
ICAS2012-11.6.3 |
Ciampa, P.D. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
Cikrikci, D. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
Clark, G. |
MICROSTRUCTURE AND
MECHANICAL PROPERTIES OF LASER CLADDING REPAIR OF AISI 4340 STEEL |
ICAS2012-12.4.4 |
Clarke, G. |
NUMERICAL AND EXPERIMENTAL
ANALYSIS OF A REPRESENTATIVE ADF HELICOPTER FUSELAGE |
ICAS2012-2.7.2 |
Classen, A. B. |
AN ASSET FOR IMPROVED
EFFICIENCY AND PUNCTUALITY IN AIR TRANSPORT |
ICAS2012-11.7.5 |
Clothier, R. A. |
THE SMART SKIES PROJECT:
ENABLING TECHNOLOGIES FOR FUTURE AIRSPACE ENVIRONMENTS |
ICAS2012-6.9.2 |
Cockram, J. D. |
DEVELOPING THE USE OF
NEURAL-NETWORK TEST TECHNOLOGY FROM AVIONICS TO WIRING SYSTEMS |
ICAS2012-12.5.1 |
Coldbeck, D. |
COMPOSITE SANDWICH PANEL
BIRDSTRIKE TESTING AND ANALYSIS |
ICAS2012-8.3.4 |
Coman, F. |
FLOW-INDUCED FLUTTER OF
SLENDER CANTILEVER HIGH-COMPLIANCE PLATES |
ICAS2012-8.10.5 |
Comendador, V. F. G. |
AIRCRAFT FLIGHT TRAJECTORY
DEVIATION IN THE STANDARD INSTRUMENT DEPARTURES. OPERATORS PENALTIES |
ICAS2012-10.10.2 |
Conser, D. P. |
VIBRATION AND AEROELASTIC CLEARANCE WORK FOR JASSM INTEGRATION ONTO THE F/A-18A/B |
ICAS2012-8.10.3 |
Consiglio, M. |
CONCEPT OF INTEGRATION FOR
UAS OPERATIONS IN THE NAS |
ICAS2012-10.7.1 |
Cooper, M. A. |
TOWARDS TRAJECTORY
PREDICTION AND OPTIMISATION FOR ENERGY EFFICIENCY OF AN AIRCRAFT WITH
ELECTRICAL AND HYDRAULIC ACTUATION SYSTEMS |
ICAS2012-6.7.3 |
Coporrella, M. |
EFFECT ON THE AERODYNAMIC
FORCING IN AN AXIAL TURBINE STAGE ON VARYING STATOR BLADE SHAPE |
ICAS2012-4.3.ST |
Coppin, G. |
A CAPABILITY FRAMEWORK FOR
MULTIPLE HETEROGENEOUS UAVS: FROM A MISSION COMMANDER'S PERSPECTIVE |
ICAS2012-9.7.3 |
Corcione, S. |
AERODYNAMIC ANALYSIS AND
DESIGN OF A TWIN-ENGINE COMMUTER
AIRCRAFT |
ICAS2012-1.6.2 |
Corke, P. |
VISUAL SERVOING APPROACH TO
COLLISION AVOIDANCE FOR AIRCRAFT |
ICAS2012-11.3.1 |
Correa, L. G. N. |
WIND TUNNEL TESTING OF
POROUS DEVICES FOR THE REDUCTION OF FLAP SIDE-EDGE NOISE |
ICAS2012-9.11.2 |
Correale, G. |
NOVEL PASSIVE AND ACTIVE
FLOW CONTROL FOR HIGH LIFT |
ICAS2012-3.7.2 |
Coughlan, P. |
BRISBANE AIRPORT'S NEW
PARALLEL RUNWAY |
ICAS2012-P8.4 |
Crawford, B. R. |
INITIAL RESULTS FROM DSTO’S
CORROSION STRUCTURAL INTEGRITY ROADMAP |
ICAS2012-12.6.1 |
Cresta, P. |
POSTBUCKLING COMPUTATION OF
LARGE STIFFENED STRUCTURES |
ICAS2012-8.1.3 |
Crites, D. C. |
DEVELOPMENT OF AN
EXPERIMENTAL TECHNIQUE FOR HIGH TEMPERATURE IMPINGEMENT STUDIES |
ICAS2012-12.6.3 |
Crossley, W. A. |
DEVELOPING OPTIMAL AIRLINE
FLEETS UNDER ENVIRONMENTAL AND CAPACITY CONSTRAINTS |
ICAS2012-7.10.1 |
Crossley, W. A. |
MEASURING SYSTEM-WIDE
IMPACTS OF NEW AIRCRAFT ON THE ENVIRONMENT |
ICAS2012-7.11.1 |
Crouse, G. L. |
ESTIMATING TIME TO LOSS OF
SEPARATION WITH UNCERTAIN POSITION AND VELOCITY MEASUREMENTS |
ICAS2012-10.7.4 |
Crowther, W. |
TETHERING
UNMANNED ROTORCRAFT FOR HIGH-ENDURANCE OPERATIONS |
ICAS2012-P1.3 |
Crump, M. |
ALL-SOURCE NAVIGATION FOR
ENHANCING UAV OPERATIONS IN GPS-DENIED ENVIRONMENTS |
ICAS2012-11.6.1 |
Crump, M. |
INTELLIGENT LANDING SYSTEM
FOR LANDING UAVS AT UNSURVEYED AIRFIELDS |
ICAS2012-11.6.2 |
Cuerno, C. |
LEGAL AND TECHNICAL
IMPLICATIONS OF THE SAFETY RECOMMENDATIONS ISSUED IN THE FINAL REPORTS OF THE
CIVIL AIR ACCIDENTS AND INCIDENTS INVESTIGATIONS |
ICAS2012-9.4.ST |
Cuerno, C. |
PRELIMINARY AERODYNAMIC
INVESTIGATION OF AN UNMANNED BOX-WING AIRCRAFT |
ICAS2012-P2.13 |
Cui, D. |
THE WORKFLOW CONSTRUCTION
AND MANAGEMENT IN AERONAUTICAL MULTIDISCIPLINARY OPTIMIZATION |
ICAS2012-2.1.2 |
Cui, D. |
THE METHOD FOR NONLINEAR
ANALYSIS OPTIMIZATION IN AERONAUTICAL RESEARCH |
ICAS2012-P1.2 |
Cui, R. H. |
RESEARCH ON CRACK GROWTH OF
MULTIPLE-SITE DAMAGED STRUCTURE |
ICAS2012-7.1.3 |
Cuzieux, F. |
MODELING OF LOSS OF TAIL
ROTOR EFFECTIVENESS CONDUCTING TO UNANTICIPATED YAW |
ICAS2012-5.10.3 |
da Silva, R. G. |
ON THE EFFECTS OF TURBULENCE
MODELING AND GRID REFINEMENT ON HIGH-LIFT CONFIGURATION AERODYNAMIC
SIMULATIONS |
ICAS2012-2.3.1 |
Danilin, A. I. |
THE NEW OPTIMALITY CRITERIA
FOR STRUCTURAL DESIGN WITH CONSTRAINING ELASTIC DISPLACEMENTS |
ICAS2012-8.7.5 |
Daoud, F. |
MULTIDISCIPLINARY AIRFRAME
DESIGN OPTIMIZATION |
ICAS2012-0.4 |
David, M. |
IMPROVED DESIGN METHODS FOR
CRASHWORTHY COMPOSITE HELICOPTER STRUCTURES |
ICAS2012-8.1.2 |
de Boer, A. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
de Boer, A. |
ACCELERATED LIFE CONSUMPTION
DUE TO THERMO-ACOUSTIC OSCILLATIONS IN GAS TURBINES: XFEM & CRACK |
ICAS2012-4.2.2 |
De Crescenzio, F. |
INNOVATION IN MAN MACHINE
INTERFACES: USE OF 3D CONFORMAL SYMBOLS IN THE DESIGN OF FUTURE HUDS (HEAD UP
DISPLAYS) |
ICAS2012-9.7.2 |
De felice, N. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
De Gaspari, A. |
NEOCASS: AN OPEN SOURCE
ENVIRONMENT FOR THE AEROELASTIC ANALYSIS AT CONCEPTUAL DESIGN LEVEL |
ICAS2012-8.10.1 |
de Lamberterie, P. |
COMPUTATIONAL ASPECTS OF
PROBABILISTIC ASSESSMENT OF UAS ROBUST AUTONOMY |
ICAS2012-9.2.2 |
de Lamberterie, P. |
EVALUATION OF ROBUST
AUTONOMY AND IMPLICATIONS ON UAS DESIGN |
ICAS2012-9.4.2 |
de Muynck, R. |
OPTIMIZING INBOUND AIRCRAFT
STREAMS USING AIRCRAFT DERIVED DATA AND RTA FUNCTIONALITY |
ICAS2012-10.4.4 |
de Muynck, R. J. |
IMPLEMENTING TIME BASED CDA
OPERATIONS IN A MEDIUM-HIGH DENSITY ATM ENVIRONMENT |
ICAS2012-10.8.1 |
de Olim, A. |
A PRACTICAL, ROUTE-BASED
APPROACH TO AIRSPACE CAPACITY MANAGEMENT |
ICAS2012-10.2.2 |
De Saint Jean, M. |
STREAMWISE AND CROSSFLOW
INSTABILITIES ON INCLINED CIRCULAR CYLINDERS |
ICAS2012-3.10.2 |
de Vries, H. |
EXPERIMENTAL/NUMERICAL
INVESTIGATION AIRFOIL WITH FLOW CONTROL BY SYNTHETIC JETS |
ICAS2012-3.7.5 |
Dehne, T. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
Deivasigamani, A. |
FLOW-INDUCED FLUTTER OF
SLENDER CANTILEVER HIGH-COMPLIANCE PLATES |
ICAS2012-8.10.5 |
DeLaurentis, D. |
DESCRIPTION AND EVALUATION
OF MULTI-THREAT TRACKING ARCHITECTURES |
ICAS2012-11.2.3 |
DeLaurentis, D. A. |
DEVELOPING OPTIMAL AIRLINE
FLEETS UNDER ENVIRONMENTAL AND CAPACITY CONSTRAINTS |
ICAS2012-7.10.1 |
Della Vecchia, P. |
AERODYNAMIC ANALYSIS AND
DESIGN OF A TWIN-ENGINE COMMUTER
AIRCRAFT |
ICAS2012-1.6.2 |
Delloue, D. |
COUPLING MECH. & THERMAL
MODELS IN PRELIMINARY DESIGN OF POWER TRANSMISSIONS DRIVEN BY THERMAL ISSUES |
ICAS2012-6.6.1 |
Deng, J. |
DESIGN OF LAMINAR
SUPERCRITICAL AIRFOILS BASED ON NAVIER-STOKES EQUATIONS |
ICAS2012-2.2.2 |
Dequand, S. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
Derrien, J. -C. |
ELECTROMECHANICAL ACTUATOR
(EMA) ADVANCED TECHNOLOGIES FOR FLIGHT CONTROLS |
ICAS2012-6.8.ST |
Desopper, A. |
MODELING OF LOSS OF TAIL
ROTOR EFFECTIVENESS CONDUCTING TO UNANTICIPATED YAW |
ICAS2012-5.10.3 |
Desse, J. -M. |
SUBSONIC WAKE FLOWS ANALYSIS
BY DIGITAL THREE-WAVELENGTHS HOLOGRAPHIC INTERFEROMETRY |
ICAS2012-3.11.3 |
Desyatnik, P. A. |
EFFECTS OF MANIPULATOR TYPE
AND FEEL SYSTEM CHARACTERISTICS ON HIGH-FREQUENCY BIODYNAMIC PILOT-AIRCRAFT
INTERACTION |
ICAS2012-5.9.3 |
Desyatnik, P. A. |
SOME ASPECTS OF MOVING-BASE
SIMULATION OF UPSET RECOVERING MANEUVER |
ICAS2012-5.9.4 |
Deutschmann, A. |
PREDICTION OF AIRPORT DELAYS
BASED ON NON-LINEAR CONSIDERATIONS OF AIRPORTS SYSTEMS |
ICAS2012-10.10.4 |
Di Meo, G. A. |
INTEROPERABILITY OF MILITARY
AIRCRAFT VERSUS FUTURE AIR NAVIGATION SYSTEM (FANS) |
ICAS2012-10.1.3 |
Dieke-Meier, F. |
THE NEED FOR A COLLISION
PREVENTION SYSTEM FOR THE PUSHBACK OF AIRCRAFT |
ICAS2012-9.10.5 |
Djojodihardjo, H. |
CONCEPTUAL DESIGN AND AERODYNAMIC STUDY OF JOINED-WING
BUSINESS JET AIRCRAFT |
ICAS2012-1.10.4 |
Djojodihardjo, H. |
CONCEPTUAL DESIGN AND
AERODYNAMIC STUDY OF BLENDED WING BODY BUSINESS JET |
ICAS2012-2.9.2 |
Djojodihardjo, H. |
COMPUTATIONAL STUDY ON THE
INFLUENCE OF COANDA JET ON AIRFOILS: TWO-DIMENSIONAL CASE |
ICAS2012-4.6.ST2 |
Doberstein, D. |
MODEL BASED DESIGN AND
EXPERIMENTAL VALIDATION OF ELECTRO-MECHANIC ACTUATOR SYSTEMS FOR A NOSE
LANDING GEAR |
ICAS2012-6.8.3 |
Dobrev, Y. |
MODEL VALIDATION OF A
TILTWING UAV IN TRANSITION PHASE APPLYING WINDTUNNEL INVESTIGATIONS |
ICAS2012-11.1.1 |
Dobrev, Y. |
CONTROL CONCEPT OF A
TILTWING UAV DURING LOW SPEED MANOEUVRING |
ICAS2012-11.1.2 |
Doi, A. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
Doig, G. |
PROGRESS IN UNDERSTANDING
TRANSONIC AND SUPERSONIC GROUND EFFECT AERODYNAMICS |
ICAS2012-10.6.3 |
Döll, C. |
AUTOPILOT
DESIGN FOR THE EOLE DEMONSTRATOR |
ICAS2012-5.3.4 |
Dolvin, D. J. |
HIFIRE: AN INTERNATIONAL COLLABORATION TO ADVANCE THE SCIENCE AND TECHNOLOGY OF HYPERSONIC FLIGHT |
ICAS2012-0.8 |
Dong, W. |
THE PERFORMANCE COMPUTATION
OF THE HOT AIR ANTI-ICING SYSTEM OF AN AERO-ENGINE CONE |
ICAS2012-2.6.2 |
Dong, W. F. |
DETERMINATION OF AIRBORNE
RECORDED PARAMETERS FOR COMPREHENSIVE FLIGHT DATA MONITORING PROGRAM |
ICAS2012-9.4.1 |
Dong, Y. |
RESEARCH ON ESTIMATING
METHOD OF FUEL AND EMISSIONS USING NEURAL NETWORKS IN LTO CYCLE FOR
PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-7.11.2 |
Donough, M. J. |
CRITICAL ASSESSMENT OF
FAILURE CRITERION FOR ADHESIVELY BONDED COMPOSITE JOINT REPAIR DESIGN |
ICAS2012-12.2.2 |
Doolan, C. J. |
EXPERIMENTAL INVESTIGATION
OF FLAT PLATE SELF-NOISE REDUCTION USING TRAILING EDGE SERRATIONS |
ICAS2012-9.11.1 |
Dorbath, F. |
A KNOWLEDGE BASED APPROACH
FOR EXTENDED PHYSICS-BASED WING MASS ESTIMATION IN EARLY DESIGN STAGES |
ICAS2012-1.1.1 |
Dragan, K. |
FATIGUE LIFE ANALYSIS OF
MAIN LANDING GEAR PULL-ROD OF THE
FIGHTER JET AIRCRAFT |
ICAS2012-12.4.3 |
Dridi, W. |
MULTI-OBJECTIVE OPTIMIZATION
OF MULTI-ELEMENT HIGH-LIFT AIRFOIL |
ICAS2012-2.3.4 |
Drobik, J. |
A RECENT HISTORY OF THE
EVOLUTION OF AUSTRALIA’S AERODYNAMICS STORE SEPARATION CAPABILITY – THROUGH
INDIGENOUS AND INTERNATIONAL PROGRAMS |
ICAS2012-10.6.4 |
Du, H. |
THE WORKFLOW CONSTRUCTION
AND MANAGEMENT IN AERONAUTICAL MULTIDISCIPLINARY OPTIMIZATION |
ICAS2012-2.1.2 |
Du, H. |
THE METHOD FOR NONLINEAR
ANALYSIS OPTIMIZATION IN AERONAUTICAL RESEARCH |
ICAS2012-P1.2 |
Duan, Z. W. |
INVESTIGATION OF PASSIVE
FLOW CONTROL METHODOLOGIES USING SST-IDDES |
ICAS2012-P2.7 |
Dubinsky, V. |
OUTLINE OF AIRCRAFT
STRUCTURE HEALTH AND USAGE MONITORING SYSTEMS AND METHODS USED FOR THEIR
REALIZATIONS |
ICAS2012-12.1.2 |
Dubois, J. |
SIMULATION OF THE FULL
COUPLING BETWEEN THE RADIATION TRANSFER AND THE AERODYNAMICS FOR HYPERSONIC REENTRY PROBES |
ICAS2012-3.8.ST |
Dubovikov, E. |
NOVEL APPROACH AND ALGORITHM
FOR SEARCHING RATIONAL NONCONVENTIONAL AIRFRAME CONCEPTS OF NEW GENERATION
AIRCRAFTS |
ICAS2012-8.8.2 |
Dubovitskiy, A. |
EXPERIMENTAL INVESTIGATIONS
OF HYDRAULIC DEVICES PERFORMANCE IN AVIATION ENGINE COMPARTMENT |
ICAS2012-P2.10 |
Duda, H. |
FLIGHT PERFORMANCE OF
LIGHTWEIGHT GYROPLANES |
ICAS2012-5.6.2 |
Duong, C. G. |
PILOT CONVECTIVE WEATHER
DECISION MAKING IN EN ROUTE AIRSPACE |
ICAS2012-10.4.3 |
Dutré, S. |
IDENTIFICATION OF HELICOPTER
GROUND RESONANCE WITH MULTI-BODY SIMULATION |
ICAS2012-8.3.2 |
Dzikus, N. |
TECHNOLOGY ASSESSMENT OF
FUTURE AIRCRAFT: SOCIO-ECO-EFFICIENCY IN CONCEPTUAL AIRCRAFT DESIGN |
ICAS2012-1.9.2 |
Dzuba, A. S. |
INVESTIGATION OF CRACK
PROPAGATION BY OPTICAL INTERFEROMETRIC MEASUREMENTS OF LOCAL DEFORMATION
RESPONSE |
ICAS2012-7.9.2 |
Efremov, A. V. |
TECHNIQUE FOR FLYING
QUALITIES AND PIO PREDICTION |
ICAS2012-5.9.2 |
Eggers and the Shefex II-Team, T. |
THE SHEFEX II EXPERIMENTAL
RE-ENTRY VEHICLE: PRESENTATION OF FLIGHT TEST RESULTS |
ICAS2012-5.4.4 |
Eggers, T. |
NUMERICAL INVESTIGATION ON
THE POTENTIAL OF STEAM COOLING FOR THE SKYLON SPACEPLANE IN HYPERSONIC FLOW |
ICAS2012-2.8.1 |
Egorov, I. |
NUMERICAL SIMULATION OF
THREE-DIMENSIONAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTION ON SHARP AND BLUNTED
FLAT PLATE |
ICAS2012-2.4.2 |
Ehmer, H. |
ICAO’S BALANCED APPROACH TO
NOISE MANAGEMENT AND ITS INFLUENCE ON THE ECONOMIC IMPACT OF AIR
TRANSPORTATION |
ICAS2012-7.10.4 |
Eitelberg, G. |
PROPELLER INDUCED GROUND
VORTEX |
ICAS2012-4.10.3 |
Ekhtiari, M. |
WAVELET-BASED ACTIVE SENSING
FOR QUANTITATIVE ASSESSMENT OF THROUGH-THICKNESS CRACK SIZE AND ANGLE IN
COMPOSITE PLATES |
ICAS2012-P3.8 |
Ellbrant, L. |
CFD OPTIMIZATION OF A
TRANSONIC COMPRESSOR USING MULTIOBJECTIVE GA AND METAMODELS |
ICAS2012-4.6.3 |
Ellström, H. |
MORE ELECTRICAL
ENVIRONMENTAL CONTROL SYSTEM SIMULATION |
ICAS2012-6.6.4 |
Elston, J. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
Enea, G. |
A COMPARISON OF
4D-TRAJECTORY OPERATIONS ENVISIONED FOR 'NEXTGEN' AND 'SESAR', SOME
PRELIMINARY FINDINGS |
ICAS2012-10.3.1 |
Enqvist, M. |
NONLINEAR AERODYNAMIC
MODELING OF UNSTABLE AIRCRAFT USING FLIGHT TEST DATA |
ICAS2012-5.10.1 |
Entzinger, J. O. |
INSIDE THE PILOTS MIND:
VISUAL INFORMATION USE IN MANUAL AIRCRAFT LANDINGS |
ICAS2012-9.7.1 |
Erdelyi, H. |
DESIGN STUDY OF AN ACTIVE
GURNEY FLAP SYSTEM FOR HELICOPTER ROTOR BLADES |
ICAS2012-6.11.1 |
Erdem, E. |
PERFORMANCE ANALYSIS OF A
SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
ICAS2012-P4.12 |
Eriksson, B. |
AIRCRAFT SYSTEM SIMULATION
FOR PRELIMINARY DESIGN |
ICAS2012-1.9.3 |
Eriksson, L. -E. |
CFD OPTIMIZATION OF A
TRANSONIC COMPRESSOR USING MULTIOBJECTIVE GA AND METAMODELS |
ICAS2012-4.6.3 |
Erlandsson, T. |
AUTOMATION GUIDELINES FOR
INTRODUCING SURVIVABILITY ANALYSIS IN FUTURE FIGHTER AIRCRAFT |
ICAS2012-9.1.1 |
Everdij, M. |
ANALYZING SEPARATION LOSS
EVENTS IN TWO-PAIRED AIRCRAFT TRAILING CONDUCTING AIRBORNE TIME SPACING BASED
CONTINUOUS DESCENT ARRIVAL |
ICAS2012-10.8.3 |
Faggiani, A. |
LAY-UP OPTIMIZATION OF
COMPOSITE PLATES TO DELAY MODE-JUMP INSTABILITIES |
ICAS2012-7.1.ST |
Falzon, B. G. |
LAY-UP OPTIMIZATION OF
COMPOSITE PLATES TO DELAY MODE-JUMP INSTABILITIES |
ICAS2012-7.1.ST |
Falzon, B. G. |
AN INVESTIGATION OF MODE I
FRACTURE TOUGHNESS USING ALIGNED CARBON-NANOTUBE FORESTS AT THE CRACK
INTERFACE |
ICAS2012-7.3.2 |
Fateev, V. A. |
EXPERIMENTAL AND NUMERICAL
STUDY OF TWO FIRST HIGHLY-LOADED STAGES OF COMPRESSORS AS A PART OF HPC AND
SEPARATE UNIT |
ICAS2012-4.6.1 |
Faugere, E. |
COUPLING MECH. & THERMAL
MODELS IN PRELIMINARY DESIGN OF POWER TRANSMISSIONS DRIVEN BY THERMAL ISSUES |
ICAS2012-6.6.1 |
Featherston, C. |
IMPROVED EXACT STRIP
POSTBUCKLING ANALYSIS FOR ANISOTROPIC PLATES WITH FIXED, FREE AND STRAIGHT
EDGES |
ICAS2012-8.2.1 |
Fedina, Y. A. |
VIBRATION STRENGTH INCREASE
OF ROTATING BLADES USING DYNAMIC SPIN RIGS |
ICAS2012-12.6.4 |
Feih, S. |
DAMAGE TOLERANCE OF Z-PINNED
COMPOSITE JOINTS |
ICAS2012-7.5.2 |
Feng, W. -C. |
A NEW METHOD OF CALCULATION
THE DELAY TIME OF MULTI-CREW MEMBER EJECTION |
ICAS2012-P6.2 |
Ferrand, P. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
Ferrand, P. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
Ferreira, L. O. F. |
AIRCRAFT EMERGENCY
EVACUATION SIMULATION USING ANT COLONY OPTIMIZATION |
ICAS2012-9.1.3 |
Feuerle, T. |
GBAS CURVED APPROACH
PROCEDURES: ADVANTAGES, CHALLENGES AND APPLICABILITY |
ICAS2012-4.9.2 |
Fezans, N. |
EMERGENCY PROPULSION-BASED
AUTOLAND SYSTEM |
ICAS2012-5.1.3 |
Fezans, N. |
A MODEL OF HORIZONTAL
TAILPLANE DAMAGE FOR USE IN FLIGHT DYNAMICS |
ICAS2012-P5.3 |
Fielding, J. P. |
BOX WING AIRCRAFT CONCEPTUAL
DESIGN |
ICAS2012-1.9.ST |
Fielding, J. P. |
PRELIMINARY STUDY OF EMA
LANDING GEAR ACTUATION |
ICAS2012-6.8.2 |
Figat, M. |
MODULAR AEROPLANE SYSTEM. A
CONCEPT AND INITIAL INVESTIGATION |
ICAS2012-1.3.2 |
Filippis, L. De |
AN INNOVATIVE MISSION
MANAGEMENT SYSTEM FOR FIXED-WING UAVS |
ICAS2012-11.7.1 |
Filsinger, J. |
ASSESSMENT OF STRUCTURAL
EFFECT OF SELECTIVE STITCHING ON COMPOSITE SKIN-STIFFENER BONDING |
ICAS2012-8.9.1 |
Fischer, M. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
Fisher, A. |
DYNAMIC SURFACE PRESSURE
MEASUREMENTS ON A FLAPPING WING IN SMOOTH AND TURBULENT FLOW |
ICAS2012-9.11.ST1 |
Fitzpatrick, I. R. |
DESIGN OF COMPOSITE
STRUCTURES FOR IMPROVED AEROELASTIC PERFORMANCE |
ICAS2012-8.4.4 |
Foenander, J. J. |
DESIGN
OF A TWO-DIMENSIONAL GASDYNAMIC NOZZLE USING MULTI-OBJECTIVE PARTICLE SWARM
OPTIMISATION |
ICAS2012-P4.8 |
Fomin, V. |
DESIGNING PRO-COMPOSITE
AIRCRAFT CONCEPTS AND LAYOUTS TO MAXIMIZE POTENTIAL BENEFITS OF HIGH SPECIFIC
STRENGTH OF CFRP |
ICAS2012-1.7.3 |
Fomin, V. P. |
STRENGTH CRITERIA
DEVELOPMENT FOR COMPOSITE STRUCTURES BASING ON SOLUTIONS SUPERPOSITION FOR
MODELS OF DIFFERENT LEVELS |
ICAS2012-7.1.2 |
Foong, K. E. |
CONCEPTUAL DESIGN AND AERODYNAMIC STUDY OF JOINED-WING
BUSINESS JET AIRCRAFT |
ICAS2012-1.10.4 |
Ford, J. J |
DESIGN OF FLIGHT AVOIDANCE
MANOEUVRE ALPHABETS FOR MIXED CENTRALISED-DECENTRALISED SEPARATION MANAGEMENT |
ICAS2012-10.7.3 |
Ford, J. J. |
FLIGHT TRIAL OF AN
ELECTRO-OPTICAL SENSE-AND-AVOID SYSTEM |
ICAS2012-11.2.1 |
Ford, J. J. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
Forrester, A. J. |
MODELLING OF A WARPING WING
FOR ENERGY CONSUMPTION MINIMIZATION |
ICAS2012-1.3.4 |
Forslund, A. |
ROBUST LIFECYCLE
OPTIMIZATION OF TURBINE COMPONENTS USING SIMULATION PLATFORMS |
ICAS2012-4.3.2 |
Fosso-Pouangue, A. |
MULTI-OBJECTIVE OPTIMIZATION
OF MULTI-ELEMENT HIGH-LIFT AIRFOIL |
ICAS2012-2.3.4 |
Francia, D. |
DESIGN ANALYSIS FOR HYBRID
PROPULSION |
ICAS2012-6.7.5 |
Francia, D. |
A
META-HEURISTIC APPROACH TO SIMULATE TAXI OPERATIONS |
ICAS2012-P8.7 |
Fransson, T. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
Freeman, D. |
METHODOLOGY FOR THE DESIGN
OF UNMANNED AIRCRAFT PRODUCT FAMILIES |
ICAS2012-9.9.2 |
Freeman, D. |
DESIGN OF UNMANNED AIR
SYSTEMS FOR USE IN SEARCH AND RESCUE IN THE NORTH ATLANTIC |
ICAS2012-9.9.3 |
Fricke, H. |
DYNAMIC TURNAROUND
MANAGEMENT IN A HIGHLY AUTOMATED AIRPORT ENVIRONMENT |
ICAS2012-10.9.2 |
Fricke, H. |
THE NEED FOR A COLLISION
PREVENTION SYSTEM FOR THE PUSHBACK OF AIRCRAFT |
ICAS2012-9.10.5 |
Fricke, H. |
INVESTIGATING THE SAFETY
IMPACT OF TIME BUFFERS IN CURRENT TMA ARRIVAL OPERATIONS |
ICAS2012-9.4.3 |
Friswell, M. I. |
COMPUTATIONAL AND
EXPERIMENTAL ANALYSIS OF THE ACTIVE MORPHING WING CONCEPT |
ICAS2012-2.5.3 |
Frousheger, D. |
THE SMART SKIES PROJECT:
ENABLING TECHNOLOGIES FOR FUTURE AIRSPACE ENVIRONMENTS |
ICAS2012-6.9.2 |
Fu, S. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
Fu, S. |
INVESTIGATION OF PASSIVE
FLOW CONTROL METHODOLOGIES USING SST-IDDES |
ICAS2012-P2.7 |
Fu, W. |
INVESTIGATION
ON PROPELLER ENGINE OPTIMUM INSTALLATION POSITION ON A SOLAR POWERED UNMANNED
AERIAL VEHICLE |
ICAS2012-2.10.5 |
Fu, W. |
EXPLORING
THE AERODYNAMIC INTERFERENCE OF PROPELLER-WING ON A SOLAR POWERED UNMANNED
AERIAL VEHICLE |
ICAS2012-9.8.3 |
Fu, Y. L |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
Fu, Y. L. |
INVESTIGATION IN THE DYNAMIC
FORCE EQUALIZATION OF DISSIMILAR REDUNDANT ACTUATION SYSTEMS OPERATING IN
ACTIVE/ACTIVE MODE |
ICAS2012-6.8.1 |
Fucke, L. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
Fucke, L. |
UNRELIABLE AIRSPEED – MAKING
VALID ASSUMPTIONS ON FLIGHT CREW PERFORMANCE |
ICAS2012-9.3.4 |
Fujimori, A. |
ESTIMATION OF AERODYNAMIC
DERIVATIVES IN AIRCRAFT MODEL USING ITERATIVE LEARNING IDENTIFICATION |
ICAS2012-5.10.5 |
Fujishiro, T. |
INVESTIGATION ON STRUCTURAL
AND AERODYNAMIC CHARACTERISTICS OF RESONANT TYPE ELASTIC FLAPPING WING |
ICAS2012-9.5.3 |
Fujita, K. |
EVALUATION OF DYNAMIC
BEHAVIOR OF A DEPLOYABLE WING UAV BY DROP TEST |
ICAS2012-P2.20 |
Fujiwara, K. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
Fukuda, Y. |
CONTINUOUS DESCENT
TRAJECTORY WITH OPTIMUM ARRIVAL TIME CONTROLLABILITY |
ICAS2012-P8.3 |
Fukuoka, K. |
FUNDAMENTAL CHARACTERISTICS
OF DECENTRALIZED AIR TRAFFIC FLOW CONTROL IN HIGH DENSITY CORRIDOR |
ICAS2012-10.7.2 |
Fukushima, Y. |
ESTIMATION OF NOISE
SHIELDING EFFECT OF NEXT-GENERATION AIRCRAFT BY A COMPUTATIONAL AEROACOUSTICS
METHOD |
ICAS2012-3.9.2 |
Funabiki, K. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
Gaffuri, M. |
NUMERICAL STUDY OF THE
REYNOLDS NUMBER EFFECT ON LOW ASPECT
RATIO WINGS AT LOW SPEED |
ICAS2012-2.10.2 |
Gaind, R. |
AN EXPERIMENTAL STUDY OF A
PULSED AIR JET AND AN ACOUSTIC SYNTHETIC JET ON A LOW SPEED TURBULENT
BOUNDARY LAYER |
ICAS2012-3.5.1 |
Galea, S. |
PROBING THE LIMITS - NEW
OPPORTUNITIES IN THERMOELASTIC STRESS ANALYSIS |
ICAS2012-12.1.1 |
Galea, S. C. |
BI-AXIAL VIBRATION ENERGY
HARVESTING FOR USE ON AEROSPACE PLATFORMS |
ICAS2012-6.7.1 |
Galinski, C. |
MODULAR AEROPLANE SYSTEM. A
CONCEPT AND INITIAL INVESTIGATION |
ICAS2012-1.3.2 |
Galinski, C. |
RESULTS OF THE GUST
RESISTANT MAV PROGRAMME |
ICAS2012-3.1.1 |
Gallego, J. M. |
LEGAL AND TECHNICAL
IMPLICATIONS OF THE SAFETY RECOMMENDATIONS ISSUED IN THE FINAL REPORTS OF THE
CIVIL AIR ACCIDENTS AND INCIDENTS INVESTIGATIONS |
ICAS2012-9.4.ST |
Gamaleri, M. |
EMERGENCY PROPULSION-BASED
AUTOLAND SYSTEM |
ICAS2012-5.1.3 |
Gao, Z. |
WING-BODY OPTIMIZATION BASED
ON MULTI-FIDELITY SURROGATE MODEL |
ICAS2012-11.10.5 |
Gao, Z. |
EXTENSIONS OF MENTER’S SST
TRANSITION MODEL TO SIMULATE HYPERSONIC AND CROSS-FLOW TRANSITION |
ICAS2012-11.4.ST |
Gao, Z. |
APPLICATION
OF TWO TRANSITION MODELS TO FLOWS AROUND AIRFOILS |
ICAS2012-2.4.4 |
Gao, Z. |
CONTROL ALLOCATION FOR
AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS DURING TAKEOFF AND LANDING PHASES |
ICAS2012-5.3.3 |
Gao, Z. H. |
STUDY
ON MODELING PILOT BEHAVIOR BY ARTIFICIAL NEURAL NETWORK |
ICAS2012-5.9.ST |
Gao, Z. -H. |
NUMERICAL SIMULATION OF
TRANSONIC SHOCK-VORTEX INTERACTION FLOW AROUND THE VFE-2 DELTA WING BASED ON
MDDES |
ICAS2012-P2.4 |
Garcia, E. |
METHODOLOGY FOR THE DESIGN
OF UNMANNED AIRCRAFT PRODUCT FAMILIES |
ICAS2012-9.9.2 |
Garcia, E. |
DESIGN OF UNMANNED AIR
SYSTEMS FOR USE IN SEARCH AND RESCUE IN THE NORTH ATLANTIC |
ICAS2012-9.9.3 |
Garcia, E. |
EVALUATING FLEXIBILITY IN
AIRPORT CAPACITY-ENHANCING TECHNOLOGY INVESTMENTS |
ICAS2012-P8.2 |
García, E. |
HALA!: TOWARDS HIGHER LEVELS
OF AUTOMATION IN ATM. POSITION PAPER -STATE OF THE ART AND RESEARCH AGENDA |
ICAS2012-10.1.1 |
García, E. |
AIRCRAFT FLIGHT TRAJECTORY
DEVIATION IN THE STANDARD INSTRUMENT DEPARTURES. OPERATORS PENALTIES |
ICAS2012-10.10.2 |
Gareev, A. M. |
MODELING OF FLUID CONDITION
OF AIRCRAFT HYDRAULIC SYSTEM |
ICAS2012-6.6.2 |
Gareyev, T. M. |
MODELING OF FLUID CONDITION
OF AIRCRAFT HYDRAULIC SYSTEM |
ICAS2012-6.6.2 |
Garrett, S. J. |
STREAMWISE AND CROSSFLOW
INSTABILITIES ON INCLINED CIRCULAR CYLINDERS |
ICAS2012-3.10.2 |
Garrett, S. J. |
ON THE EFFECT OF DISTRIBUTED
ROUGHNESS ON TRANSITION OVER ROTOR-STATOR DEVICES |
ICAS2012-3.10.4 |
Garry, K. P. |
TIME DEPENDENT ANALYSIS OF A
RECTANGULAR SYNTHETIC JET |
ICAS2012-3.7.1 |
Gauci, J. |
CORRESPONDENCE AND
CLUSTERING METHODS FOR IMAGE-BASED WING-TIP COLLISION AVOIDANCE TECHNIQUES |
ICAS2012-9.10.4 |
Geesing, I. J. A. K. |
EXPERIMENTAL/NUMERICAL
INVESTIGATION AIRFOIL WITH FLOW CONTROL BY SYNTHETIC JETS |
ICAS2012-3.7.5 |
Gehre, R. M. |
THERMAL NON-EQUILIBRIUM
EFFECTS IN RADICAL FARMING SCRAMJETS |
ICAS2012-11.4.1 |
Gehre, R. M. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
Gehri, A. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
George, G. |
FINITE ELEMENT SIMULATION OF
CRACK PROPAGATION IN MILITARY AIRCRAFT COATINGS |
ICAS2012-7.2.3 |
Gerardo Castro, M. P. |
MULTIDISCIPLINARY DESIGN AND
FLIGHT TESTING OF A REMOTE GAS/PARTICLE AIRBORNE SENSOR SYSTEM |
ICAS2012-6.10.4 |
Ghadiri, B. |
NONLINEAR AEROELASTIC
ANALYSIS OF SWEPT WINGS IN COMPRESSIBLE FLOW VIA THE HARMONIC BALANCE METHOD |
ICAS2012-8.7.1 |
Ghorbani, K. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
Giacobello, M. |
NUMERICAL STUDY ON THE
EFFECT OF VARYING SPANWISE TWIST ON LOW-REYNOLDS-NUMBER FLAPPING FLIGHT |
ICAS2012-2.5.1 |
Gibbon, R. |
COMPOSITE SANDWICH PANEL
BIRDSTRIKE TESTING AND ANALYSIS |
ICAS2012-8.3.4 |
Gires, E. |
PERFORMANCE TEST OF A
SMALL-SCALE TURBOJET ENGINE RUNNING ON A PALM OIL BIODIESEL - JET A BLEND |
ICAS2012-4.8.1 |
Gluchshenko, O. |
OPTIMIZATION OF RUNWAY
CAPACITY UTILIZATION IN THE CASE OF GENERAL PARETO CURVE |
ICAS2012-10.3.4 |
Go, T. H. |
FLEXIBLE WING AERODYNAMICS
AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.1 |
Go, T. H. |
EXPERIMENTAL INVESTIGATION
OF A BI-PLANE MICRO AIR VEHICLE |
ICAS2012-3.3.4 |
Goda, Y. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
Goetzendorf-Grabowski, T. G. |
MADO – SOFTWARE PACKAGE FOR
HIGH ORDER MULTIDISCIPLINARY AIRCRAFT
DESIGN AND OPTIMIZATION |
ICAS2012-1.9.4 |
Goizueta, N. G. |
AN EXPERIMENTAL AND
NUMERICAL STUDY OF THE EFFECT OF NOSE BLUNTING ON A CONICAL NOSED BODY AT
TRANSONIC SPEED |
ICAS2012-2.8.3 |
Golia, C. |
AEROTHERMODYNAMIC FIELD PAST
A REENTRY CAPSULE FOR SAMPLE RETURN MISSIONS |
ICAS2012-3.8.1 |
Gollnick, V. |
A KNOWLEDGE BASED APPROACH
FOR EXTENDED PHYSICS-BASED WING MASS ESTIMATION IN EARLY DESIGN STAGES |
ICAS2012-1.1.1 |
Gollnick, V. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
Gollnick, V. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
Gollnick, V. |
SYSTEM ANALYSIS OF
PROGNOSTICS AND HEALTH MANAGEMENT SYSTEMS FOR FUTURE TRANSPORT AIRCRAFT |
ICAS2012-12.3.1 |
Gollnick, V. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
Golzad, I. |
FINDING TUNING FREQUENCY OF
SYMMETRIC AND ANTI-SYMMETRIC LAMB WAVES USING FEM |
ICAS2012-P3.6 |
Goman, M. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
Goman, M. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
Gong, C. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
Gonzalez, F. |
HYBRID GAME EVOLUTIONARY
ALGORITHM FOR MISSION PATH PLANNING OF AERIAL SURVEY TASKS |
ICAS2012-11.7.3 |
Gonzalez, F. |
A CAPABILITY FRAMEWORK FOR
MULTIPLE HETEROGENEOUS UAVS: FROM A MISSION COMMANDER'S PERSPECTIVE |
ICAS2012-9.7.3 |
Gonzalez, L. F. |
ROBUST AERODYNAMIC DESIGN
OPTIMISATION OF MORPHING AEROFOIL/WING USING DISTRIBUTED MOGA |
ICAS2012-11.10.3 |
Gonzalez, L. F. |
DESIGN, SIMULATION AND
ANALYSIS OF A PARALLEL HYBRID-ELECTRIC PROPULSION SYSTEM FOR UNMANNED AERIAL
VEHICLES |
ICAS2012-4.5.1 |
Gonzalez, L. F. |
MULTIDISCIPLINARY DESIGN AND
FLIGHT TESTING OF A REMOTE GAS/PARTICLE AIRBORNE SENSOR SYSTEM |
ICAS2012-6.10.4 |
Gooden, J. H. M. |
THE EFFECT OF CROSSWIND ON
ENGINE INGESTION DURING TAKEOFFS FROM WATER CONTAMINATED RUNWAYS |
ICAS2012-9.1.2 |
Gooding, C. L. |
PILOT CONVECTIVE WEATHER
DECISION MAKING IN EN ROUTE AIRSPACE |
ICAS2012-10.4.3 |
Goodwin, A. |
AGEING AIRCRAFT SYSTEMS
& COST EFFECTIVE SAFETY |
ICAS2012-12.3.2 |
Gopal, M. |
PRODUCTION
OF BIO-FUEL FROM ALGAE BIOMASS, NANNOCHLOROPSIS OCULATA, FOR ADDITION TO
KEROSENE JET A-1 |
ICAS2012-8.6.4 |
Goraj, Z. |
DESIGN AND CONFIGURATION
LAYOUTS OF AN ADVANCED LONG ENDURANCE UAV- LESSONS LEARNT AFTER FLIGHT
TESTING |
ICAS2012-1.11.3 |
Gorbushin, A. R. |
AN EXPERIENCE OF USING
NUMERICAL METHODS IN EXPERIMENTAL INVESTIGATIONS OF TsAGI |
ICAS2012-P2.6 |
Gores, I. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
Gosse, J. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
Gostelow, J. P. |
STREAMWISE AND CROSSFLOW
INSTABILITIES ON INCLINED CIRCULAR CYLINDERS |
ICAS2012-3.10.2 |
Gotseluk, T. B. |
COMPUTATIONAL AND
EXPERIMENTAL RESEARCH OF BOLT JOINTS OF METAL AND COMPOSITE IN AIRFRAMES |
ICAS2012-8.4.ST |
Gowree, E. R. |
RECENT DEVELOPMENTS TO THE
VISCOUS GARABEDIAN AND KORN METHOD |
ICAS2012-2.11.3 |
Gowree, E. R. |
A COMPUTATIONAL STUDY OF THE
AERODYNAMICS OF A SPINNING CYLINDER IN CROSSFLOW OF HIGH REYNOLDS NUMBER |
ICAS2012-3.11.2 |
Grawunder, M. |
FLOW CHARACTERISTICS OF A
HELICOPTER FUSELAGE CONFIGURATION INCLUDING A ROTATING ROTOR HEAD |
ICAS2012-2.7.3 |
Greco, P. C. |
THE INFLUENCE OF DEMOISELLE
AIRCRAFT ON LIGHT AND GENERAL AVIATION DESIGN |
ICAS2012-1.7.ST |
Greco, P. C. |
TRAILING EDGE TREATMENT TO
ENHANCE HIGH LIFT SYSTEM PERFORMANCE |
ICAS2012-3.2.3 |
Grendysa, W. |
DESIGN AND CONFIGURATION
LAYOUTS OF AN ADVANCED LONG ENDURANCE UAV- LESSONS LEARNT AFTER FLIGHT
TESTING |
ICAS2012-1.11.3 |
Grigoryev, M. A. |
FLIGHT TESTS OF TRANSPORT
AIRCRAFT UPSET RECOVERY TECHNIQUES AND THE SYSTEM OF INFORMATION SUPPORT OF
CREW |
ICAS2012-5.1.1 |
Grilli, A. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
Grinev, K. N. |
EFFECTS OF MANIPULATOR TYPE
AND FEEL SYSTEM CHARACTERISTICS ON HIGH-FREQUENCY BIODYNAMIC PILOT-AIRCRAFT
INTERACTION |
ICAS2012-5.9.3 |
Groen, E. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
Grondel, S. |
AEROELASTIC SIMULATION OF
FLEXIBLE FLAPPING WING BASED ON STRUCTURAL FEM AND QUASI-STEADY AERODYNAMIC
MODEL |
ICAS2012-8.5.1 |
Grunewald, E. |
DELPHI SURVEY 'LEVEL OF
SERVICE FOR AVIATION INFRASTRUCTURE MARKETS?' |
ICAS2012-10.2.3 |
Gubanov, A. A. |
NUMERICAL RESEARCH OF THE
AIR INTAKE LOCATION INFLUENCE ONTO THE HIGH-SPEED AIRCRAFT PERFORMANCE |
ICAS2012-P2.1 |
Guerrero, M. J. |
LEGAL AND TECHNICAL
IMPLICATIONS OF THE SAFETY RECOMMENDATIONS ISSUED IN THE FINAL REPORTS OF THE
CIVIL AIR ACCIDENTS AND INCIDENTS INVESTIGATIONS |
ICAS2012-9.4.ST |
Guglieri, G. |
AN INNOVATIVE MISSION
MANAGEMENT SYSTEM FOR FIXED-WING UAVS |
ICAS2012-11.7.1 |
Guillaume, M. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
Gulbis, A. A. |
MODELING OF FLUID CONDITION
OF AIRCRAFT HYDRAULIC SYSTEM |
ICAS2012-6.6.2 |
Gunnion, A. J. |
CRITICAL ASSESSMENT OF
FAILURE CRITERION FOR ADHESIVELY BONDED COMPOSITE JOINT REPAIR DESIGN |
ICAS2012-12.2.2 |
Guo, R. |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
Guo, W. G. |
THE DYNAMIC BEHAVIOR OF
FUNCTIONALLY GRADED PLATES UNDER THE IMPACT LOADING |
ICAS2012-7.7.3 |
Gurak, D. |
METHODS FOR EVALUATION OF
AIRCRAFT MASS DISTRIBUTION |
ICAS2012-1.1.3 |
Gurak, D. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
Gustafsson, P. |
EXTERNAL AERODYNAMIC
PRESSURE LOADS FOR A RIGID FIGHTER AIRCRAFT, A COMPARISON BETWEEN PSP AND CFD |
ICAS2012-10.6.2 |
Gutierrez, L. B. |
UAS DESIGN REQUIREMENTS FOR
OPERATION IN COLOMBIAN MOUNTAIN ENVIRONMENTS |
ICAS2012-1.8.ST |
Hadda, J. El |
NOVEL PASSIVE AND ACTIVE
FLOW CONTROL FOR HIGH LIFT |
ICAS2012-3.7.2 |
Hahn, M. |
BOUNDARY LAYER TRANSITION
DETECTION USING TEMPERATURE SENSITIVE PAINT IN THE ARA TRANSONIC WIND TUNNEL |
ICAS2012-3.4.2 |
Haikola, T. |
DIARC PLASMA COATING FOR
RELIABLE AND DURABLE STRUCTURAL BONDING OF METALS |
ICAS2012-7.2.1 |
Halfmann, N. |
THE DEVELOPMENT OF PRODUCT
AND ASSEMBLY CONCEPTS FOR AIRCRAFT CABIN INTEGRATION |
ICAS2012-9.9.1 |
Hamid, M. F. A. |
COMPUTATIONAL STUDY ON THE
INFLUENCE OF COANDA JET ON AIRFOILS: TWO-DIMENSIONAL CASE |
ICAS2012-4.6.ST2 |
Hamidiyanfar, A. |
AN
OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES |
ICAS2012-6.5.ST |
Han, B. |
FINITE ELEMENT SIMULATION OF
CRACK PROPAGATION IN MILITARY AIRCRAFT COATINGS |
ICAS2012-7.2.3 |
Han, Z. H. |
COMPARISON OF INFILL
SAMPLING CRITERIA IN KRIGING-BASED AERODYNAMIC OPTIMIZATION |
ICAS2012-11.10.ST |
Han, Z. -H. |
MULTIDISCIPLINARY EVALUATION
OF TRUSS-BRACED WING FOR FUTURE GREEN AIRCRAFT |
ICAS2012-1.10.ST |
Han, Z. -H. |
DESIGN OF LAMINAR
SUPERCRITICAL AIRFOILS BASED ON NAVIER-STOKES EQUATIONS |
ICAS2012-2.2.2 |
Hantrais-Gervois, J. -L. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
Hara, T. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
Harada, A. |
FLIGHT TRAJECTORY
OPTIMIZATION FOR AN EFFICIENT AIR TRANSPORTATION SYSTEM |
ICAS2012-5.8.3 |
Haraguchi, S. |
ANALYTICAL INVESTIGATIONS ON
LIGHT-WEIGHT STRUCTURES FOR SATELLITE STRUCTURAL FRAME APPLICATIONS THROUGH
3D MODELING |
ICAS2012-7.8.3 |
Haraldsdottir, A. |
THE GENERALIZED ARRIVAL
PLANNER (GARP): MODELING AND ANALYSIS FOR ARRIVAL PLANNING |
ICAS2012-10.9.3 |
Harel, M. |
A PERSONAL PLANE AIR
TRANSPORTATION SYSTEM: THE PPLANE PROJECT |
ICAS2012-10.5.1 |
Harin, E. G. |
METHODS AND FACILITIES TO BE
USED TO EVALUATE THE AIRCRAFT FLIGHT AND NAVIGATION EQUIPMENT IN FLIGHT TESTS |
ICAS2012-5.6.3 |
Harribey, T. |
MODELING OF THE INTERACTION
BETWEEN A TURBULENT FLOW AND AN ABLATABLE MATERIAL |
ICAS2012-3.8.2 |
Harris, J. |
ON THE EFFECT OF DISTRIBUTED
ROUGHNESS ON TRANSITION OVER ROTOR-STATOR DEVICES |
ICAS2012-3.10.4 |
Harrison, T. J. |
INITIAL RESULTS FROM DSTO’S
CORROSION STRUCTURAL INTEGRITY ROADMAP |
ICAS2012-12.6.1 |
Harrison, T. J. |
INTERGRANULAR CORROSION
PROTOCOL DEVELOPMENT FOR 7075-T651 EXTRUSION |
ICAS2012-P3.3 |
Hartley, D. L. |
DEVELOPMENT OF AN INTEGRATED
INFORMATION MANAGEMENT SYSTEM FOR AIRCRAFT STRUCTURAL TEST PROGRAMS |
ICAS2012-9.2.1 |
Harvey, J. |
FLEXIBILITY OF AN ORITHOPTER
WING TESTED IN A WIND-TUNNEL |
ICAS2012-12.5.3 |
Harvey, J. R. |
HARDWARE-IN-THE-LOOP
SIMULATION OF FUEL-CELL-BASED HYBRID-ELECTRICAL UAV PROPULSION |
ICAS2012-4.5.2 |
Harvey, J. R. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
Haselbach, F. |
HOT END TECHNOLOGY FOR
ADVANCED, LOW EMISSION LARGE CIVIL AIRCRAFT ENGINES |
ICAS2012-4.10.2 |
Hashimoto, A. |
NUMERICAL STUDY OF THE
EFFECTS OF CROSS-WIND ON THE JET BLAST DEFORMATION |
ICAS2012-10.10.3 |
Hashimoto, A. |
AUTOMATIC HANDLING OF
DEFECTIVE SURFACE GEOMETRY WITHIN GRID GENERATION FOR NAVIER-STOKES
COMPUTATION |
ICAS2012-2.11.1 |
Hashimoto, A. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
Hassan, S. |
EFFECT ON THE AERODYNAMIC
FORCING IN AN AXIAL TURBINE STAGE ON VARYING STATOR BLADE SHAPE |
ICAS2012-4.3.ST |
Hatanaka, K. |
A FULLY AUTOMATED CAD-BASED
FRAMEWORK FOR SHAPE OPTIMIZATION |
ICAS2012-11.10.1 |
Hatano, T. |
CONTINUOUS DESCENT
TRAJECTORY WITH OPTIMUM ARRIVAL TIME CONTROLLABILITY |
ICAS2012-P8.3 |
Hattori, S. |
EXPERIMENTAL STUDY OF
SUPERSONIC INLET FOR SUPPRESSION OF BUZZ IN SUBCRITICAL OPERATION |
ICAS2012-6.2.1 |
Haucke, F. |
ACTIVE
SEPARATION CONTROL ON A 2D HIGH-LIFT WING SECTION TOWARDS HIGH REYNOLDS
NUMBER APPLICATION |
ICAS2012-3.5.3 |
Hawkins, S. C. |
AN INVESTIGATION OF MODE I
FRACTURE TOUGHNESS USING ALIGNED CARBON-NANOTUBE FORESTS AT THE CRACK
INTERFACE |
ICAS2012-7.3.2 |
Hazbon, O. |
UAS DESIGN REQUIREMENTS FOR
OPERATION IN COLOMBIAN MOUNTAIN ENVIRONMENTS |
ICAS2012-1.8.ST |
He, J. |
ANALYTICAL INVESTIGATIONS ON
LIGHT-WEIGHT STRUCTURES FOR SATELLITE STRUCTURAL FRAME APPLICATIONS THROUGH
3D MODELING |
ICAS2012-7.8.3 |
He, Y. H. |
ENGINEERING FAILURE MODES
AND FRACTURE CHARACTERISTICS OF SINGLE CRYSTAL SUPERALLOY BLADES |
ICAS2012-4.2.ST |
He, Y. T. |
RESEARCH ON CRACK GROWTH OF
MULTIPLE-SITE DAMAGED STRUCTURE |
ICAS2012-7.1.3 |
Hecker, P. |
DYNAMIC SEPARATION MINIMA
COUPLED WITH WAKE VORTEX PREDICTIONS IN DEPENDENT RUNWAY CONFIGURATIONS |
ICAS2012-10.4.2 |
Hecker, P. |
GBAS CURVED APPROACH
PROCEDURES: ADVANTAGES, CHALLENGES AND APPLICABILITY |
ICAS2012-4.9.2 |
Heib, S. |
THE ONERA ELSA CFD SOFTWARE
: INPUT FROM RESEARCH AND FEEDBACK FROM INDUSTRY |
ICAS2012-2.1.1 |
Heider, A. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
Heitzmann, M. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
Helldin, T. |
AUTOMATION GUIDELINES FOR
INTRODUCING SURVIVABILITY ANALYSIS IN FUTURE FIGHTER AIRCRAFT |
ICAS2012-9.1.1 |
Heltsch, N. |
ASSESSMENT OF STRUCTURAL
EFFECT OF SELECTIVE STITCHING ON COMPOSITE SKIN-STIFFENER BONDING |
ICAS2012-8.9.1 |
Hendrick, P. |
DESIGN AND AERO-ELASTIC
OPTIMISATION OF THE STRUCTURE OF THE LAPCAT A2 MACH 5 AIRLINER |
ICAS2012-8.4.3 |
Henner, M. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
Hermetz, J. |
EOLE, AN INNOVATIVE FLYING
SCALE DEMONSTRATOR FOR AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS |
ICAS2012-1.11.2 |
Hernando, J. -L. |
CARRIER SUITABILITY OF
LAND-BASED AIRCRAFT |
ICAS2012-1.1.ST |
Higashino, K. |
DEVELOPMENT OF A SMALL-SCALE
SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED |
ICAS2012-1.2.2 |
Higashiyama, Y. |
DEVELOPMENT OF LAPTOP PC
TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |
ICAS2012-9.10.ST |
Higuchi, T. |
COLLISION AVOIDANCE OF
INDOOR FLYING DOUBLE TETRAHEDRON HEXA-ROTORCRAFT |
ICAS2012-11.5.1 |
Hinckley, S. |
DISTRIBUTED
OPTICAL FIBRE SMART SENSORS FOR ADVANCE SENSING SYSTEMS IN AEROSPACE VEHICLES |
ICAS2012-P6.7 |
Hino, T. |
REAL TIME PATH PLANNING
METHOD OF AIRCRAFT FORMATIONS |
ICAS2012-11.7.2 |
Hiraoka, K. |
COMPARISON OF PERFORMANCE OF
PROPELLER BLADES BY DIFFERENCE IN PLANAR SHAPE |
ICAS2012-4.6.ST1 |
Hishida, M. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
Ho, D. |
INVESTIGATION OF LOW THRUST
TO WEIGHT RATIO ROTATIONAL CAPACITY OF ASYMMETRIC MONO-WING CONFIGURATIONS |
ICAS2012-1.4.3 |
Hoeijmakers, H. W. M. |
NUMERICAL METHOD FOR ICE
ACCRETION ON 3D WINGS |
ICAS2012-2.6.1 |
Hoeijmakers, H. W. M. |
EXPERIMENTAL/NUMERICAL
INVESTIGATION AIRFOIL WITH FLOW CONTROL BY SYNTHETIC JETS |
ICAS2012-3.7.5 |
Hoffler, K. |
CONCEPT OF INTEGRATION FOR
UAS OPERATIONS IN THE NAS |
ICAS2012-10.7.1 |
Holsten, J. |
MODEL VALIDATION OF A
TILTWING UAV IN TRANSITION PHASE APPLYING WINDTUNNEL INVESTIGATIONS |
ICAS2012-11.1.1 |
Holsten, J. |
CONTROL CONCEPT OF A
TILTWING UAV DURING LOW SPEED MANOEUVRING |
ICAS2012-11.1.2 |
Hölzel, N. B. |
SYSTEM ANALYSIS OF
PROGNOSTICS AND HEALTH MANAGEMENT SYSTEMS FOR FUTURE TRANSPORT AIRCRAFT |
ICAS2012-12.3.1 |
Honda, M. |
D-SEND PROJECT FOR LOW SONIC
BOOM DESIGN TECHNOLOGY |
ICAS2012-1.2.1 |
Honnery, D. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
Hordé, T. |
APACHE : INTEGRATED HYBRID
FUEL CELL SYSTEM FOR 2-SEAT ALL ELECTRIC AIRCRAFTS PROPULSION |
ICAS2012-6.7.4 |
Hornung, M. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
Hornung, M. |
AIRPORT CAPACITY
REPRESENTATION BASED ON AIRSIDE SIMULATIONS |
ICAS2012-10.10.1 |
Hornung, M. |
A SCENARIO-BASED APPROACH TO
DEVELOP REPRESENTATIVE TRAFFIC ENVIRONMENTS FOR OPERATIONAL AIRCRAFT
EVALUATION |
ICAS2012-6.3.1 |
Hospers, J. M. |
NUMERICAL METHOD FOR ICE
ACCRETION ON 3D WINGS |
ICAS2012-2.6.1 |
Hospodar, P. |
GLOBAL OPTIMIZATION OF
TWO-DIMENSIONAL HIGH LIFT AERODYNAMIC SYSTEM |
ICAS2012-11.10.2 |
Hospodar, P. |
STABILIZATION OF
LONGITUDINAL AIRCRAFT MOTION USING MODEL PREDICTIVE CONTROL AND EXACT
LINEARIZATION |
ICAS2012-P5.11 |
Hosseini Kordkheili, S. A. |
APPLICATION
OF SINGULAR VALUE DECOMPOSITION IN COMPONENT MODE SYNTHESIS WITH EXPERIMENTAL
APPROACH |
ICAS2012-8.11.3 |
Hosseini, A. |
AN
APPROXIMATE ENGINEERING METHOD FOR AERODYNAMIC HEATING SOLUTION AROUND BLUNT
BODY NOES |
ICAS2012-11.4.4 |
Hou, J. |
PRE-STRESSED MODAL ANALYSIS
OF A TURBINE SPACER |
ICAS2012-P4.11 |
Hou, M. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
Hou, T. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
Howarth, D. |
OPTIMIZING DESIGN
SPECIFICATIONS FROM AIRCRAFT MARKET ECONOMICS |
ICAS2012-6.3.4 |
Hsu, H. -T. |
THE AFFECT OF SCREEN SIZE ON
MISSION COMMANDER’S SITUATION AWARENESS |
ICAS2012-9.7.5 |
Hu, Y. |
AERODYNAMICS ANALYSIS OF
CYCLOIDAL ROTOR |
ICAS2012-2.7.1 |
Huang, J. B. |
INVESTIGATION OF PASSIVE
FLOW CONTROL METHODOLOGIES USING SST-IDDES |
ICAS2012-P2.7 |
Huang, J. -T. |
NUMERICAL SIMULATION OF
TRANSONIC SHOCK-VORTEX INTERACTION FLOW AROUND THE VFE-2 DELTA WING BASED ON
MDDES |
ICAS2012-P2.4 |
Huang, L. |
WING-BODY OPTIMIZATION BASED
ON MULTI-FIDELITY SURROGATE MODEL |
ICAS2012-11.10.5 |
Huang, W. |
RESEARCH FOR JET FLOW INFLUENCES TO WING-MOUNTED CIVIL
AIRCRAFT AERODYNAMIC CHARACTERISTICS |
ICAS2012-2.9.1 |
Huang, X. |
CRACK NUCLEATION MODELING IN
NOTCHED SPECIMEN SUBJECTED TO HIGH FATIGUE LOADING |
ICAS2012-7.7.4 |
Huby, G. M. |
DEVELOPING THE USE OF
NEURAL-NETWORK TEST TECHNOLOGY FROM AVIONICS TO WIRING SYSTEMS |
ICAS2012-12.5.1 |
Hue, D. |
AUTOMATED CHAIN FOR
AERODYNAMIC COMPUTATIONS MEETING AIRCRAFT TRIMMING REQUIREMENTS |
ICAS2012-2.10.1 |
Hühne, C. |
SEMI-ANALYTICAL SPRING-IN
ANALYSIS TO COUNTERACT CFRP MANUFACTURING DEFORMATIONS BY TOOL COMPENSATION |
ICAS2012-8.2.2 |
Hui, K. |
INNOVATIVE
MOISTURE/ICING-RESISTANT FLUSH AIR DATA SYSTEM |
ICAS2012-6.5.1 |
Hung, J. Y. -C. |
DESIGN, SIMULATION AND
ANALYSIS OF A PARALLEL HYBRID-ELECTRIC PROPULSION SYSTEM FOR UNMANNED AERIAL
VEHICLES |
ICAS2012-4.5.1 |
Hwang, Y. H. |
TERRAIN REFERENCED UAV
NAVIGATION WITH LIDAR - A COMPARISON OF SEQUENTIAL PROCESSING AND BATCH
PROCESSING ALGORITHMS |
ICAS2012-P5.7 |
Idris, A. |
PERFORMANCE TEST OF A
SMALL-SCALE TURBOJET ENGINE RUNNING ON A PALM OIL BIODIESEL - JET A BLEND |
ICAS2012-4.8.1 |
Idris, A. C. |
EXPERIMENTAL STUDIES ON
MICRO-VORTEX GENERATORS IN HYPERSONIC FLOW |
ICAS2012-3.5.2 |
Inada, Y. |
AERODYNAMIC CHARACTERISTICS
OF A BIRD-LIKE ASSEMBLED WING |
ICAS2012-P2.22 |
Inada, Y. |
FORMATION SHAPE CONTROL OF
UNMANNED AIR VEHICLES |
ICAS2012-P5.8 |
Inada, Y. |
GUST RESPONSE ANALYSIS IN
THE FLIGHT FORMATION OF UNMANNED AIR VEHICLES |
ICAS2012-P5.9 |
Inagawa, N. |
DEVELOPMENT OF OBSERVATIONAL
SYSTEM WITH UNMANNED FLIGHT SYSTEM |
ICAS2012-P5.10 |
Inoue, Y. |
DEVELOPMENT OF SUPERSONIC
NATURAL LAMINAR FLOW WING DESIGN SYSTEM USING CFD-BASED INVERSE METHOD |
ICAS2012-2.2.1 |
Ireland, M. |
DEVELOPMENT OF NAVIGATION
ALGORITHMS FOR NAP-OF-THE-EARTH UAV FLIGHT IN A CONSTRAINED URBAN ENVIRONMENT |
ICAS2012-11.9.1 |
Isa, M. D. |
DAMAGE TOLERANCE OF Z-PINNED
COMPOSITE JOINTS |
ICAS2012-7.5.2 |
Ishida, T. |
AUTOMATIC HANDLING OF
DEFECTIVE SURFACE GEOMETRY WITHIN GRID GENERATION FOR NAVIER-STOKES
COMPUTATION |
ICAS2012-2.11.1 |
Ishikawa, H. |
DEVELOPMENT OF SUPERSONIC
NATURAL LAMINAR FLOW WING DESIGN SYSTEM USING CFD-BASED INVERSE METHOD |
ICAS2012-2.2.1 |
Ishikawa, T. |
LESSONS LEARNED IN FULL
COMPOSITE AERO-STRUCTURES DEVELOPMENT IN JAPAN |
ICAS2012-0.3 |
Ishiko, K. |
NUMERICAL STUDY OF THE
EFFECTS OF CROSS-WIND ON THE JET BLAST DEFORMATION |
ICAS2012-10.10.3 |
Ishiko, K. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
Ishmuratov, F. |
ANALYSIS OF STATIC AND
DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW |
ICAS2012-8.10.4 |
Ishmuratov, F. |
AEROELASTIC
MULTIDISCIPLINARY ANALYSIS OF THE FIN
WITH INNOVATIVE ADAPTIVE CONTROL |
ICAS2012-8.7.4 |
Isikdogan, O. |
METHODS FOR EVALUATION OF
AIRCRAFT MASS DISTRIBUTION |
ICAS2012-1.1.3 |
Isikveren, A. T. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
Isikveren, A. T. |
PROGRESS AND PERSPECTIVES OF
ELECTRIC AIR TRANSPORT |
ICAS2012-8.6.1 |
Isogai, K. |
NUMERICAL SIMULATION OF
SHOCK-STALL FLUTTER OF A HIGH-ASPECT-RATIO FORWARD-SWEPT WING |
ICAS2012-8.10.2 |
Isogai, K. |
INVESTIGATION ON STRUCTURAL
AND AERODYNAMIC CHARACTERISTICS OF RESONANT TYPE ELASTIC FLAPPING WING |
ICAS2012-9.5.3 |
Isozumi, R. |
THEORETICAL AND EXPERIMENTAL
INVESTIGATIONS ON CHOKING PHENOMENA OF AXISYMMETRIC CONVERGENT NOZZLE FLOW |
ICAS2012-P2.11 |
Itabashi, N. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
Itano, K. |
DEVELOPMENT AND EVALUATION
OF FATIGUE AND DROWSINESS PREDICTOR |
ICAS2012-9.6.1 |
Ito, T. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
Ito, T. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
Itoh, E. |
ANALYZING SEPARATION LOSS
EVENTS IN TWO-PAIRED AIRCRAFT TRAILING CONDUCTING AIRBORNE TIME SPACING BASED
CONTINUOUS DESCENT ARRIVAL |
ICAS2012-10.8.3 |
Iuspa, L. |
DESIGN OF MASS SAVING
CONFIGURATIONS FOR WINGED REENTRY VEHICLES |
ICAS2012-1.5.3 |
Ivanov, D. |
NUMERICAL SIMULATION OF
THREE-DIMENSIONAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTION ON SHARP AND BLUNTED
FLAT PLATE |
ICAS2012-2.4.2 |
Ivanov, M. J. |
INTERDISCIPLINARY COMPLEX
DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES |
ICAS2012-4.3.3 |
Iwahori, Y. |
EVALUATION ON DISCRETE
SOURCE DAMAGES OF CFRP STIFFENED PANELS |
ICAS2012-7.7.1 |
Jahanmiri, M. |
MEASUREMENTS AND PREDICTION
OF LAMINAR-TURBULENT TRANSITION AT HIGH FREE-STREAM TURBULENCE & PRESSURE
GRADIENTS |
ICAS2012-3.10.5 |
Janardhana, M. |
EFFECT OF OFF-NORMAL LOADING
ON THE BOND STRENGTH MEASUREMENT OF BONDED REPAIRS |
ICAS2012-12.2.1 |
Janardhana, M. |
MICROSTRUCTURE AND
MECHANICAL PROPERTIES OF LASER CLADDING REPAIR OF AISI 4340 STEEL |
ICAS2012-12.4.4 |
Janik, W. |
A COMPOSITE AND
METAL JOINT FOR A PROPELLER BLADE ROOT |
ICAS2012-7.5.3 |
Jansen, D. |
NOVEL PASSIVE AND ACTIVE
FLOW CONTROL FOR HIGH LIFT |
ICAS2012-3.7.2 |
Jarvis, R. A. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
Jebens, K. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
Jemitola, P. O. |
BOX WING AIRCRAFT CONCEPTUAL
DESIGN |
ICAS2012-1.9.ST |
Jeong, M. -S. |
AEROELASTIC ANALYSIS FOR
HELICOPTER ROTOR BLADES IN HOVER AND FORWARD FLIGHTS |
ICAS2012-11.5.3 |
Jeung, I. -S. |
EFFECT OF VENT MIXER TO
MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
ICAS2012-P4.4 |
Ji, P. -B. |
MULTIDISCIPLINARY EVALUATION
OF TRUSS-BRACED WING FOR FUTURE GREEN AIRCRAFT |
ICAS2012-1.10.ST |
Jia, H. |
A CASE STUDY OF ARRIVAL AND
DEPARTURE MANAGERS COOPERATION FOR REDUCING AIRBORNE HOLDING TIMES AT
DESTINATION AIRPORTS |
ICAS2012-10.1.ST |
Jia, M. |
ANALYZING AND MODELING OF
JAMMING DESTROY FACTOR |
ICAS2012-P6.1 |
Jia, Y. -Y. |
NUMERICAL STUDY ON RESIDUAL
THERMAL STRESSES IN CARBON FIBRE PULLOUT |
ICAS2012-7.3.1 |
Jiang, X. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
Jimin, K. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
Jo, M. -S. |
VERIFICATION OF OPTICAL
PAYLOAD CFRP STRUCTURE FOR SATELLITE THROUGH ANALYSIS AND SPACE QUALIFICATION
TEST |
ICAS2012-P3.9 |
Johanning, A. |
NOVEL LOW-FLYING
PROPELLER-DRIVEN AIRCRAFT CONCEPT FOR REDUCED DIRECT OPERATING COSTS AND
EMISSIONS |
ICAS2012-1.10.5 |
John, S. |
FLOW-INDUCED FLUTTER OF
SLENDER CANTILEVER HIGH-COMPLIANCE PLATES |
ICAS2012-8.10.5 |
Johnson, W. W. |
PILOT CONVECTIVE WEATHER
DECISION MAKING IN EN ROUTE AIRSPACE |
ICAS2012-10.4.3 |
Jon, A. |
A COMPUTATIONAL STUDY ON THE
DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF
THE VEHICLE |
ICAS2012-2.2.ST |
Jonas, M. |
DESIGN AND CONFIGURATION
LAYOUTS OF AN ADVANCED LONG ENDURANCE UAV- LESSONS LEARNT AFTER FLIGHT
TESTING |
ICAS2012-1.11.3 |
Jones, D. P. |
COMPUTATIONAL AND
EXPERIMENTAL ANALYSIS OF THE ACTIVE MORPHING WING CONCEPT |
ICAS2012-2.5.3 |
Jones, M. |
QUANTITATIVE FRACTOGRAPHY
MARKERS FOR DETERMINING FATIGUE CRACK GROWTH RATES IN ALUMINIUM AND TITANIUM
AIRCRAFT STRUCTURES |
ICAS2012-12.4.1 |
Jones, M. B. |
FLEXIBILITY OF AN ORITHOPTER
WING TESTED IN A WIND-TUNNEL |
ICAS2012-12.5.3 |
Jones, R. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
Joo, S. |
OPTIMIZATION OF
TWO-DIMENSIONAL WING IN GROUND EFFECT CONSIDERING AERODYNAMIC CENTRE OF
HEIGHT AND LIFT |
ICAS2012-P2.15 |
Joosten, M. W. |
IMPROVED DESIGN METHODS FOR
CRASHWORTHY COMPOSITE HELICOPTER STRUCTURES |
ICAS2012-8.1.2 |
Jothiprasad, G. |
THE EFFECT OF PLASMA
ACTUATORS ON TIP CLEARANCE FLOWS IN COMPRESSOR ROTORS |
ICAS2012-4.4.1 |
Jouannet, C. |
RECYCLING OLD WEIGHT
ASSESSMENT METHODS AND GIVING THEM NEW LIFE IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS2012-1.1.2 |
Jouannet, C. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
Joulia, A. |
AIRCRAFT 4D CONTRACT BASED
OPERATION: THE 4DCO-GC PROJECT |
ICAS2012-10.3.3 |
Joyce, K. J. |
THE AUSTRALIAN ARMY AND
UNMANNED AERIAL VEHICLES… 2O YEARS AND FINALLY IN-SERVICE |
ICAS2012-1.11.1 |
Jun, B. -E. |
AUTOPILOT DESIGN FOR AN
AGILE MISSILE USING L1 ADAPTIVE BACKSTEPPING CONTROL |
ICAS2012-P5.4 |
Jung, S. |
COMPARATIVE EVALUATION OF
ICING ON AERODYNAMIC SURFACES |
ICAS2012-3.4.3 |
Jupp, J. A. |
21ST CENTURY CHALLENGES FOR
THE DESIGN OF PASSENGER AIRCRAFT |
ICAS2012-1.10.1 |
Juracka, J. |
THE DETERMINATION OF
DELAMINATION STRAIN ENERGY RELEASE RATE OF COMPOSITE BI-MATERIAL INTERFACE |
ICAS2012-7.4.1 |
Justin, C. Y. |
A COMPETITIVE AND
REAL-OPTIONS FRAMEWORK FOR THE ECONOMIC ANALYSIS OF LARGE AEROSPACE PROGRAMS |
ICAS2012-6.3.2 |
Kachel, S. |
A NEW APPROACH TO IDENTIFICATION AND OPTIMIZATION OF AIRFOILS
BY USING THE COMBINATORIAL-CYCLIC METHOD |
ICAS2012-P2.24 |
Kaden, M. |
DESIGN, ANALYSIS AND
MANUFACTURING OF A THERMOPLASTIC UD CF-PEEK SLAT |
ICAS2012-6.1.1 |
Kaden, M. |
REPAIR CONCEPT SUPPORTED BY
LASER REMOVAL AND INDUCTIVE HEATING |
ICAS2012-7.6.1 |
Kafyeke, F. |
BOMBARDIER
C-SERIES AIRCRAFT DEVELOPMENT |
ICAS2012-0.5 |
Kageyama, K. |
A BASIC STUDY ON EFFICIENCY IN JAPANESE
AIRSPACE |
ICAS2012-10.2.1 |
Kajikawa, Y. |
SCIENCE AND TECHNOLOGY MAP
ANALYSIS OF AEROSPACE ENGINEERING |
ICAS2012-P7.1 |
Kalinin, D. V. |
OPTIMAL HIGH-SPEED
HELICOPTER TRANSMISSION DESIGNS |
ICAS2012-P4.13 |
Kameda, M. |
EXPERIMENTAL STUDY OF
SUPERSONIC INLET FOR SUPPRESSION OF BUZZ IN SUBCRITICAL OPERATION |
ICAS2012-6.2.1 |
Kameda, M. |
PERFORMANCE EVALUATION OF A
BOUNDARY-LAYER DIVERTER FOR SUPERSONIC PROPULSION SYSTEM |
ICAS2012-6.2.2 |
Kappel, E. |
SEMI-ANALYTICAL SPRING-IN
ANALYSIS TO COUNTERACT CFRP MANUFACTURING DEFORMATIONS BY TOOL COMPENSATION |
ICAS2012-8.2.2 |
Kappenberger, C. |
HMIAC – SURVEY ON
HUMAN-MACHINE INTERACTION IN AIRCRAFT COCKPITS |
ICAS2012-9.7.4 |
Kappenberger, C. |
A MODEL OF HORIZONTAL
TAILPLANE DAMAGE FOR USE IN FLIGHT DYNAMICS |
ICAS2012-P5.3 |
Kaps, R. |
DESIGN, DEVELOPMENT AND
MANUFACTURING OF THE ALCAS CFRP DOOR SURROUND STRUCTURE |
ICAS2012-8.8.1 |
Karas, O. V. |
AN EXPERIENCE IN AERODYNAMIC
DESIGN OF TRANSPORT AIRCRAFT |
ICAS2012-2.9.3 |
Karas, O. V. |
ANALYSIS OF STATIC AND
DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW |
ICAS2012-8.10.4 |
Katupitiya, J. |
DESIGN OF A mu SYNTHESIS
CONTROLLER TO STABILIZE AN UNMANNED HELICOPTER |
ICAS2012-11.5.2 |
Katupitiya, J. |
A GREY-BOX SYSTEM
IDENTIFICATION PROCEDURE FOR SCALE MODEL HELICOPTERS BASED ON
FREQUENCY-DOMAIN ESTIMATION METHODS |
ICAS2012-11.9.ST |
Kaushik, B. |
DESIGN METHODS FOR AN
UNCONVENTIONAL SPLIT WING AIRCRAFT CONFIGURATION |
ICAS2012-1.3.1 |
Kawaguchi, J. |
GUIDANCE AND CONTROL LAW FOR
D-SEND#2 |
ICAS2012-5.3.1 |
Kawamura, N. |
INSTABILITY CHARACTERISTICS
OF SHOCK WAVES AHEAD OF A HEMISPHERICAL SHELL AT SUPERSONIC SPEEDS |
ICAS2012-11.4.2 |
Kawasaki, S. |
INTEGRATED DESIGN METHOD OF
A ROCKET ENGINE TURBOPUMP SUB-SYSTEM FOR SUPPRESSING ROTOR LATERAL VIBRATION |
ICAS2012-4.3.4 |
Kawazoe, H. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
Keane, A. J. |
MODELLING OF A WARPING WING
FOR ENERGY CONSUMPTION MINIMIZATION |
ICAS2012-1.3.4 |
Keck, R. |
REPAIR CONCEPT SUPPORTED BY
LASER REMOVAL AND INDUCTIVE HEATING |
ICAS2012-7.6.1 |
Keck, R. A. |
DESIGN, ANALYSIS AND
MANUFACTURING OF A THERMOPLASTIC UD CF-PEEK SLAT |
ICAS2012-6.1.1 |
Kellner, S. |
AN ASSET FOR IMPROVED
EFFICIENCY AND PUNCTUALITY IN AIR TRANSPORT |
ICAS2012-11.7.5 |
Kelly, D. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
Kelly, D. |
DIRECTIONAL ENHANCEMENT OF
COMPOSITE STRUCTURES ENERGY ABSORPTION USING MAGNETORHEOLOGICAL FLUIDS |
ICAS2012-7.8.1 |
Kelly, D. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
Kelly, D. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
Kennedy, D. |
IMPROVED EXACT STRIP
POSTBUCKLING ANALYSIS FOR ANISOTROPIC PLATES WITH FIXED, FREE AND STRAIGHT
EDGES |
ICAS2012-8.2.1 |
Kestek, H. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
Khaletskiy, Y. |
STUDY ON NOISE OF COUNTER
ROTATING FAN MODELS AT CIAM ANECHOIC CHAMBER |
ICAS2012-3.9.4 |
Kharkovsky, S. V. |
INTERDISCIPLINARY COMPLEX
DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES |
ICAS2012-4.3.3 |
Khodagolian, V. |
AN EXPERIMENTAL STUDY OF A
PULSED AIR JET AND AN ACOUSTIC SYNTHETIC JET ON A LOW SPEED TURBULENT
BOUNDARY LAYER |
ICAS2012-3.5.1 |
Khrabrov, A. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
Khrabrov, A. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
Kim, C. -H. |
EFFECT OF VENT MIXER TO
MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
ICAS2012-P4.4 |
Kim, D. -J. |
VERIFICATION OF OPTICAL
PAYLOAD CFRP STRUCTURE FOR SATELLITE THROUGH ANALYSIS AND SPACE QUALIFICATION
TEST |
ICAS2012-P3.9 |
Kim, E. T. |
HIDDEN MARKOV MODEL
PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
ICAS2012-P6.5 |
Kim, J. -H. |
A COMPUTATIONAL STUDY ON THE
DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF
THE VEHICLE |
ICAS2012-2.2.ST |
Kim, J. -H. |
UAV COLLISION AVOIDANCE VIA
OPTIMAL TRAJECTORY GENERATION METHOD |
ICAS2012-P5.5 |
Kim, J. W. |
MODELING OF NO AND OH
INFRARED RADIATION ON A CONVERGENT-DIVERGENT NOZZLE |
ICAS2012-P4.6 |
Kim, K. -H. |
A COMPUTATIONAL STUDY ON THE
DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF
THE VEHICLE |
ICAS2012-2.2.ST |
Kim, K. -S. |
A PEG-BASED ASCENDING
GUIDANCE ALGORITHM FOR RAMJET-POWERED VEHICLES |
ICAS2012-5.7.4 |
Kim, S. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
Kim, S. T. |
CFD COMPUTATION OF THE
GROUND EFFECT ON AIRPLANE WITH HIGH ASPECT RATIO WING |
ICAS2012-P2.23 |
Kim, T. H. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
Kim, Y. |
MULTIPLE UAV FORMATION
RECONFIGURATION WITH COLLISION AVOIDANCE GUIDANCE VIA DIFFERENTIAL GEOMETRY
CONCEPT |
ICAS2012-11.2.2 |
Kim, Y. |
VISION-BASED UAV GUIDANCE
AND ESTIMATION FOR AERIAL TARGET TRACKING |
ICAS2012-11.3.2 |
Kim, Y. |
CFD COMPUTATION OF THE
GROUND EFFECT ON AIRPLANE WITH HIGH ASPECT RATIO WING |
ICAS2012-P2.23 |
Kim, Y. -H. |
TIME DEPENDENT ANALYSIS OF A
RECTANGULAR SYNTHETIC JET |
ICAS2012-3.7.1 |
Kimmel, R. |
HIFIRE-1 BOUNDARY-LAYER
TRANSITION MEASUREMENTS |
ICAS2012-3.10.3 |
Kindervater, C. |
IMPROVED DESIGN METHODS FOR
CRASHWORTHY COMPOSITE HELICOPTER STRUCTURES |
ICAS2012-8.1.2 |
Kiper, T. |
METHODS FOR EVALUATION OF
AIRCRAFT MASS DISTRIBUTION |
ICAS2012-1.1.3 |
Kistan, T. |
A PRACTICAL, ROUTE-BASED
APPROACH TO AIRSPACE CAPACITY MANAGEMENT |
ICAS2012-10.2.2 |
Kleine, H. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
Kleineberg, M. |
SENSOR AND
REAL-TIME-PROCESS-SIMULATION GUIDED AUTOCLAVE PROCESS CONTROL FOR COMPOSITE
PRODUCTION |
ICAS2012-6.1.2 |
Kleineberg, M. |
DESIGN, DEVELOPMENT AND
MANUFACTURING OF THE ALCAS CFRP DOOR SURROUND STRUCTURE |
ICAS2012-8.8.1 |
Klingauf, U. |
OPERATIONAL
HUMAN-IN-THE-LOOP INTEGRATION OF 4D ARRIVAL GUIDANCE |
ICAS2012-5.8.1 |
Kmiecik, M. |
A HIGHLY EXPANDABLE LOW-COST
OPEN-SOURCE UAV SYSTEM WITH HIGH ON-BOARD PROCESSING POWER |
ICAS2012-1.8.1 |
Kobayashi, R. |
DEVELOPMENT OF LAPTOP PC
TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |
ICAS2012-9.10.ST |
Koh, T. M. |
DAMAGE TOLERANCE OF Z-PINNED
COMPOSITE JOINTS |
ICAS2012-7.5.2 |
Kok, J. |
HYBRID GAME EVOLUTIONARY
ALGORITHM FOR MISSION PATH PLANNING OF AERIAL SURVEY TASKS |
ICAS2012-11.7.3 |
Kok, M. |
LABORATORY TESTING OF INSECT
CONTAMINATION FOR LAMINAR FLOW APPLICATIONS USING AN INSECT-IMPACT TEST
FACILITY |
ICAS2012-3.4.4 |
Kolesnikov, E. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
Kölzsch, A. |
VORTEX FLOW MANIPULATION ON
GENERIC DELTA WING CONFIGURATIONS |
ICAS2012-3.6.4 |
Kondakov, I. |
DESIGNING PRO-COMPOSITE
AIRCRAFT CONCEPTS AND LAYOUTS TO MAXIMIZE POTENTIAL BENEFITS OF HIGH SPECIFIC
STRENGTH OF CFRP |
ICAS2012-1.7.3 |
Konno, A. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
Kontis, K. |
EXPERIMENTAL STUDIES ON
MICRO-VORTEX GENERATORS IN HYPERSONIC FLOW |
ICAS2012-3.5.2 |
Kontis, K. |
PERFORMANCE ANALYSIS OF A
SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
ICAS2012-P4.12 |
Kopylov, I. A. |
METHODS AND FACILITIES TO BE
USED TO EVALUATE THE AIRCRAFT FLIGHT AND NAVIGATION EQUIPMENT IN FLIGHT TESTS |
ICAS2012-5.6.3 |
Korn, B. |
FLIGHT TESTING OF NOISE
ABATING RNP PROCEDURES AND STEEP APPROACHES |
ICAS2012-4.9.1 |
Korovin, A. A. |
TECHNIQUE FOR FLYING
QUALITIES AND PIO PREDICTION |
ICAS2012-5.9.2 |
Koshelenko, A. V. |
TECHNIQUE FOR FLYING
QUALITIES AND PIO PREDICTION |
ICAS2012-5.9.2 |
Kosushkin, K. G. |
ADVANCED AEROSPACE SYSTEMS
WITH INTERCONTINENTAL AND GLOBAL RANGE OF FLIGHT |
ICAS2012-1.5.2 |
Kouchi, T. |
EFFECT OF VENT MIXER TO
MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
ICAS2012-P4.4 |
Kovalev, I. E. |
ADVANCED AEROSPACE SYSTEMS
WITH INTERCONTINENTAL AND GLOBAL RANGE OF FLIGHT |
ICAS2012-1.5.2 |
Kozakiewicz, A. |
A NEW APPROACH TO IDENTIFICATION AND OPTIMIZATION OF AIRFOILS
BY USING THE COMBINATORIAL-CYCLIC METHOD |
ICAS2012-P2.24 |
Kozharinov, E.V. |
OPTIMAL HIGH-SPEED
HELICOPTER TRANSMISSION DESIGNS |
ICAS2012-P4.13 |
Kozhemyako, P. G. |
EXPERIMENTAL AND NUMERICAL
STUDY OF TWO FIRST HIGHLY-LOADED STAGES OF COMPRESSORS AS A PART OF HPC AND
SEPARATE UNIT |
ICAS2012-4.6.1 |
Krause, D. |
THE DEVELOPMENT OF PRODUCT
AND ASSEMBLY CONCEPTS FOR AIRCRAFT CABIN INTEGRATION |
ICAS2012-9.9.1 |
Krombholz, C. |
IMPROVING THE PRODUCTION
QUALITY OF THE ADVANCED AUTOMATED FIBER PLACEMENT PROCESS BY MEANS OF ONLINE
PATH CORRECTION |
ICAS2012-6.1.3 |
Kruchkov, A. N. |
THE INSTABILITY OF THE
PIPELINE DUE TO TRANSPORTING FLUID’S PRESSURE RIPPLES |
ICAS2012-8.11.1 |
Krupa, V. G |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
Krus, P. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
Krus, P. |
AIRCRAFT SYSTEM SIMULATION
FOR PRELIMINARY DESIGN |
ICAS2012-1.9.3 |
Krus, P. |
MORE ELECTRICAL
ENVIRONMENTAL CONTROL SYSTEM SIMULATION |
ICAS2012-6.6.4 |
Kruse, M. |
MISSION AND ECONOMIC
ANALYSIS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY |
ICAS2012-1.7.4 |
Krzysiak, A. |
HELICOPTER RETREATING BLADE
STALL CONTROL USING SELF-SUPPLYING AIR JET VORTEX |
ICAS2012-3.6.2 |
Kubo, D. |
TRANSITION FLIGHT OF QUAD
TILT WING VTOL UAV |
ICAS2012-11.1.3 |
Kubo, D. |
HIGH ANGLE OF ATTACK FLIGHT
CONTROL OF A TAIL-SITTER UNMANNED AIRCRAFT |
ICAS2012-11.8.2 |
Kubo, K. |
THEORETICAL AND EXPERIMENTAL
INVESTIGATIONS ON CHOKING PHENOMENA OF AXISYMMETRIC CONVERGENT NOZZLE FLOW |
ICAS2012-P2.11 |
Kuenz, A. |
IMPLEMENTING TIME BASED CDA
OPERATIONS IN A MEDIUM-HIGH DENSITY ATM ENVIRONMENT |
ICAS2012-10.8.1 |
Kufieta, K. |
OPTIMIZATION OF A NEW
MULTI-PURPOSE UAS FOR SCIENTIFIC APPLICATIONS USING AERODYNAMIC
RECONFIGURATION |
ICAS2012-11.6.4 |
Kügler, D. |
FLIGHT TESTING OF NOISE
ABATING RNP PROCEDURES AND STEEP APPROACHES |
ICAS2012-4.9.1 |
Kuhn, H. |
PROGRESS AND PERSPECTIVES OF
ELECTRIC AIR TRANSPORT |
ICAS2012-8.6.1 |
Kuijk, J. van |
HOW A HIGH-SCHOOL STUDENT
BUILT THE FIRST DUTCH HUMAN POWERED AIRCRAFT |
ICAS2012-1.6.3 |
Kunze, T. |
DYNAMIC TURNAROUND
MANAGEMENT IN A HIGHLY AUTOMATED AIRPORT ENVIRONMENT |
ICAS2012-10.9.2 |
Kurdelski, M. |
FATIGUE LIFE ANALYSIS OF
MAIN LANDING GEAR PULL-ROD OF THE
FIGHTER JET AIRCRAFT |
ICAS2012-12.4.3 |
Kurdelski, M. |
INTRODUCTION OF A STRUCTURE
INTEGRITY PROGRAM FOR A MILITARY TRAINER AIRCRAFT |
ICAS2012-12.6.2 |
Kurdila, A. |
A
LEAP IN LEARNED BIO-INSPIRED FLIGHT |
ICAS2012-9.5.ST |
Kurihara, J. |
AERODYNAMIC CHARACTERISTICS
OF A BIRD-LIKE ASSEMBLED WING |
ICAS2012-P2.22 |
Kuzmina, S. I. |
ANALYSIS OF STATIC AND
DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW |
ICAS2012-8.10.4 |
Kwak, D. |
NUMERICAL STUDY OF THE
REYNOLDS NUMBER EFFECT ON LOW ASPECT
RATIO WINGS AT LOW SPEED |
ICAS2012-2.10.2 |
Kwak, D. |
STUDIES ON IMPROVEMENT OF
NONLINEAR PITCHING MOMENT CHARACTERISTICS OF CRANKED-ARROW WING |
ICAS2012-3.2.1 |
Kwiek, A. |
MODULAR AEROPLANE SYSTEM. A
CONCEPT AND INITIAL INVESTIGATION |
ICAS2012-1.3.2 |
Kwon, O. J. |
MODELING OF NO AND OH
INFRARED RADIATION ON A CONVERGENT-DIVERGENT NOZZLE |
ICAS2012-P4.6 |
La Rocca, G. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
La Rocca, G. |
THE DESIGN AND ENGINEERING
ENGINE. TOWARDS A MODULAR SYSTEM FOR COLLABORATIVE AIRCRAFT DESIGN |
ICAS2012-6.3.3 |
la Rocca, G. |
AUTOMATIC FLATTENING OF THREE-DIMENSIONAL WIRING HARNESSES FOR
MANUFACTURING |
ICAS2012-6.4.2 |
Labit, S. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
Lahur, P. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
Lahur, P. R. |
AUTOMATIC HANDLING OF
DEFECTIVE SURFACE GEOMETRY WITHIN GRID GENERATION FOR NAVIER-STOKES
COMPUTATION |
ICAS2012-2.11.1 |
Lai, J. |
FLIGHT TRIAL OF AN
ELECTRO-OPTICAL SENSE-AND-AVOID SYSTEM |
ICAS2012-11.2.1 |
Lai, J. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
Lam, J. K.-W. |
COLD FUEL TEST RIG TO
INVESTIGATE ICE ACCRETION ON DIFFERENT PUMP INLET FILTER-MESH SCREENS |
ICAS2012-6.5.2 |
Lambregts, A. A. |
FLY-BY-WIRE AUGMENTED MANUAL
CONTROL - BASIC DESIGN CONSIDERATIONS |
ICAS2012-5.4.1 |
Langen, T. H. M. |
THE DESIGN AND ENGINEERING
ENGINE. TOWARDS A MODULAR SYSTEM FOR COLLABORATIVE AIRCRAFT DESIGN |
ICAS2012-6.3.3 |
Langkamp, D. |
TETHERING
UNMANNED ROTORCRAFT FOR HIGH-ENDURANCE OPERATIONS |
ICAS2012-P1.3 |
Lanzillo, G. |
DESIGN OF MASS SAVING
CONFIGURATIONS FOR WINGED REENTRY VEHICLES |
ICAS2012-1.5.3 |
Larsson, R. |
NONLINEAR AERODYNAMIC
MODELING OF UNSTABLE AIRCRAFT USING FLIGHT TEST DATA |
ICAS2012-5.10.1 |
Lau, F. J. P. |
ON SOUND GENERATION BY
MOVING SURFACES AND CONVECTED SOURCES IN A FLOW |
ICAS2012-P2.8 |
Laurenzi, S. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
Lawson, C. P. |
COLD FUEL TEST RIG TO
INVESTIGATE ICE ACCRETION ON DIFFERENT PUMP INLET FILTER-MESH SCREENS |
ICAS2012-6.5.2 |
Lawson, C. P. |
TOWARDS TRAJECTORY
PREDICTION AND OPTIMISATION FOR ENERGY EFFICIENCY OF AN AIRCRAFT WITH
ELECTRICAL AND HYDRAULIC ACTUATION SYSTEMS |
ICAS2012-6.7.3 |
Le Tallec, C. |
AIRCRAFT 4D CONTRACT BASED
OPERATION: THE 4DCO-GC PROJECT |
ICAS2012-10.3.3 |
Le Tallec, C. |
A PERSONAL PLANE AIR
TRANSPORTATION SYSTEM: THE PPLANE PROJECT |
ICAS2012-10.5.1 |
Ledogar, J. |
EOLE, AN INNOVATIVE FLYING
SCALE DEMONSTRATOR FOR AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS |
ICAS2012-1.11.2 |
Lee, C. H. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
Lee, C. -H. |
AUTOPILOT DESIGN FOR AN
AGILE MISSILE USING L1 ADAPTIVE BACKSTEPPING CONTROL |
ICAS2012-P5.4 |
Lee, D. S. |
ROBUST AERODYNAMIC DESIGN
OPTIMISATION OF MORPHING AEROFOIL/WING USING DISTRIBUTED MOGA |
ICAS2012-11.10.3 |
Lee, I. |
AEROELASTIC ANALYSIS FOR
HELICOPTER ROTOR BLADES IN HOVER AND FORWARD FLIGHTS |
ICAS2012-11.5.3 |
Lee, J. |
OPTIMIZATION OF
TWO-DIMENSIONAL WING IN GROUND EFFECT CONSIDERING AERODYNAMIC CENTRE OF
HEIGHT AND LIFT |
ICAS2012-P2.15 |
Lee, J. W. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
Lee, K. -J. |
VERIFICATION OF OPTICAL
PAYLOAD CFRP STRUCTURE FOR SATELLITE THROUGH ANALYSIS AND SPACE QUALIFICATION
TEST |
ICAS2012-P3.9 |
Lee, M. |
EFFECT OF OFF-NORMAL LOADING
ON THE BOND STRENGTH MEASUREMENT OF BONDED REPAIRS |
ICAS2012-12.2.1 |
Lee, S. -T. |
A METHOD FOR THE EVALUATION
OF ELECTROMECHANICAL ACTUATOR SYSTEMS USING EXERGY |
ICAS2012-6.6.3 |
Lee, Y. J. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
Lefebvre, T. |
AIRCRAFT CONCEPTUAL DESIGN
IN A MULTI-LEVEL, MULTI-FIDELITY, MULTI-DISCIPLINARY OPTIMIZATION PROCESS |
ICAS2012-1.6.4 |
Lehmkuehler, K. |
DESIGN AND TEST OF A UAV
BLENDED WING BODY CONFIGURATION |
ICAS2012-1.8.3 |
Lehner, S. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
Lei, W. |
MULTI-OBJECTIVE AERODYNAMIC
OPTIMIZATION DESIGN OF MULTI-ELEMENT AIRFOIL USING KRIGING MODEL |
ICAS2012-2.3.ST |
Leipold, A. |
ICAO’S BALANCED APPROACH TO
NOISE MANAGEMENT AND ITS INFLUENCE ON THE ECONOMIC IMPACT OF AIR
TRANSPORTATION |
ICAS2012-7.10.4 |
Lemmens, Y. |
DESIGN STUDY OF AN ACTIVE
GURNEY FLAP SYSTEM FOR HELICOPTER ROTOR BLADES |
ICAS2012-6.11.1 |
Lemmens, Y. |
IDENTIFICATION OF HELICOPTER
GROUND RESONANCE WITH MULTI-BODY SIMULATION |
ICAS2012-8.3.2 |
Lemmens, Y. |
RELIABILITY ANALYSIS OF
AIRCRAFT SYSTEM ARCHITECTURES |
ICAS2012-P9.1 |
Leski, A. |
FATIGUE LIFE ANALYSIS OF
MAIN LANDING GEAR PULL-ROD OF THE
FIGHTER JET AIRCRAFT |
ICAS2012-12.4.3 |
Leski, A. |
INTRODUCTION OF A STRUCTURE
INTEGRITY PROGRAM FOR A MILITARY TRAINER AIRCRAFT |
ICAS2012-12.6.2 |
Lesser, A. |
NUMERICAL INVESTIGATION OF
THE EFFECT OF INFLOW DISTORTIONS ON TRANSONIC AXIAL COMPRESSOR STAGES WITH 2D
AND 3D CALCULATIONS |
ICAS2012-4.6.2 |
Levandowski, C. P. |
ROBUST LIFECYCLE
OPTIMIZATION OF TURBINE COMPONENTS USING SIMULATION PLATFORMS |
ICAS2012-4.3.2 |
Levinski, O. |
APPLICATION OF DYNAMIC
PRESSURE MEASUREMENT FOR EMPENNAGE BUFFET |
ICAS2012-3.4.1 |
Levora, T. |
ADVANCED DISPLAY AND
POSITION ANGLES MEASUREMENT SYSTEMS |
ICAS2012-P6.3 |
Lewe, J. -H. |
A METHOD FOR THE EVALUATION
OF ELECTROMECHANICAL ACTUATOR SYSTEMS USING EXERGY |
ICAS2012-6.6.3 |
Li, D. |
IMPROVED PARTICLE SWARM
OPTIMIZATION BASED ON SOCIAL MODEL FOR AERODYNAMIC DESIGN |
ICAS2012-11.10.4 |
Li, D. |
NUMERICAL INVESTIGATION OF
FLOW OVER MULTI-ELEMENT AIRFOILS WITH LIFT-ENHANCING TABS |
ICAS2012-2.3.2 |
Li, D. |
NUMERICAL STUDY OF PITCHING
OSCILLATION EFFECT ON AERODYNAMIC CHARACTERISTICS OVER ASYMMETRIC VORTEX
STRUCTURE OF SLENDER REVOLUTION |
ICAS2012-2.5.2 |
Li, G. |
RESEARCH ON FAILURE
SIMULATION OF CIVIL AIRCRAFT FLIGHT MANAGEMENT SYSTEM |
ICAS2012-5.6.4 |
Li, H. |
A NEW APPROACH FOR RE-ENTRY
VEHICLE TRAJECTORY PLANNING AND GUIDANCE |
ICAS2012-5.7.5 |
Li, H. |
THE GLARE EVALUATION METHOD
FOR CIVIL AIRPLANE FLIGHT DECK |
ICAS2012-9.3.3 |
Li, H. |
MANEUVERING TARGET TRACKING
BASED ON THE EKF |
ICAS2012-P5.2 |
Li, J. |
INVESTIGATION
ON PROPELLER ENGINE OPTIMUM INSTALLATION POSITION ON A SOLAR POWERED UNMANNED
AERIAL VEHICLE |
ICAS2012-2.10.5 |
Li, J. |
EXPLORING
THE AERODYNAMIC INTERFERENCE OF PROPELLER-WING ON A SOLAR POWERED UNMANNED
AERIAL VEHICLE |
ICAS2012-9.8.3 |
Li, L. |
INFLUENCE OF FLAPPING WING
UNSTEADY MOTION ON AERODYNAMIC PERFORMANCE OF HORIZONTAL TAIL |
ICAS2012-2.7.5 |
Li, M. |
ENHANCING THE "LAST
MILE" COMMUNICATIONS AT AIRPORTS |
ICAS2012-10.10.5 |
Li, W. |
PRELIMINARY STUDY OF EMA
LANDING GEAR ACTUATION |
ICAS2012-6.8.2 |
Li, Y. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
Li, Y. |
LCF BEHAVIOR AND LIFE
EVALUATION OF A SINGLE CRYSTAL NICKEL BASE SUPERALLOY UNDER DIFFERENT DWELL
CONDITION |
ICAS2012-7.3.3 |
Li, Y. |
STRUCTURAL
INTEGRITY ANALYSIS AND TEST OF FATIGUE CRITICAL LOCATION OF MA60 REGIONAL JET |
ICAS2012-7.9.4 |
Li, Z. |
CHARACTERISTICS
OF AN 80-DEG SWEPT DELTA WING IN WING ROCK OR FREE YAWING |
ICAS2012-3.1.ST1 |
Li, Z. |
RESEARCH ON FAILURE
SIMULATION OF CIVIL AIRCRAFT FLIGHT MANAGEMENT SYSTEM |
ICAS2012-5.6.4 |
Li, Z. |
A GENERAL FOOTPRINT
GENERATION APPROACH FOR LIFTING RE-ENTRY VEHICLE |
ICAS2012-5.7.2 |
Li, Z. |
ANGLE OF ATTACK OPERATION
ZONE ANALYSIS AND DESIGN FOR LIFTING ENTRY |
ICAS2012-5.7.3 |
Li, Z. |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
Liao, M. |
PROBABILISTIC RISK ANALYSIS
FOR AIRCRAFT STRUCTURES WITH LIMITED IN-SERVICE DAMAGES |
ICAS2012-7.9.3 |
Liao, Y. |
ANGLE OF ATTACK OPERATION
ZONE ANALYSIS AND DESIGN FOR LIFTING ENTRY |
ICAS2012-5.7.3 |
Liauzun, C. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
Liebers, N. |
SENSOR AND
REAL-TIME-PROCESS-SIMULATION GUIDED AUTOCLAVE PROCESS CONTROL FOR COMPOSITE
PRODUCTION |
ICAS2012-6.1.2 |
Lieser, J. |
IMPROVED MODELLING OF
VORTICAL MIXING FOR THE SIMULATION OF EFFICIENT PROPULSION SYSTEMS |
ICAS2012-4.10.1 |
Liew, K. E. |
PRODUCTION
OF BIO-FUEL FROM ALGAE BIOMASS, NANNOCHLOROPSIS OCULATA, FOR ADDITION TO
KEROSENE JET A-1 |
ICAS2012-8.6.4 |
Lim, D. |
DESIGN OF UNMANNED AIR
SYSTEMS FOR USE IN SEARCH AND RESCUE IN THE NORTH ATLANTIC |
ICAS2012-9.9.3 |
Lim, D. W. |
METHODOLOGY FOR THE DESIGN
OF UNMANNED AIRCRAFT PRODUCT FAMILIES |
ICAS2012-9.9.2 |
Lim, S. H. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
Lim, S. H. |
DIRECTIONAL ENHANCEMENT OF
COMPOSITE STRUCTURES ENERGY ABSORPTION USING MAGNETORHEOLOGICAL FLUIDS |
ICAS2012-7.8.1 |
Lim, S. H. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
Lim, S.-H. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
Lin, P. |
CONTROL-ORIENTED MODELING
AND ANALYSIS OF AERO-THERMO-ELASTIC-PROPULSION HYPERSONIC VEHICLE |
ICAS2012-1.5.1 |
Linde, P. |
ASSESSMENT OF STRUCTURAL
EFFECT OF SELECTIVE STITCHING ON COMPOSITE SKIN-STIFFENER BONDING |
ICAS2012-8.9.1 |
Linke, F. |
MISSION AND ECONOMIC
ANALYSIS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY |
ICAS2012-1.7.4 |
Liu, C. K |
ENGINEERING FAILURE MODES
AND FRACTURE CHARACTERISTICS OF SINGLE CRYSTAL SUPERALLOY BLADES |
ICAS2012-4.2.ST |
Liu, C. K. |
FRACTURE
ANALYSIS OF BLADE DOVETAIL OF TC11 TITANIUM ALLOY |
ICAS2012-P4.7 |
Liu, D. -B. |
THE FABRICATION AND
CHARACTERIZATION OF TiO2 UV DETECTOR |
ICAS2012-7.3.ST |
Liu, G. |
CHARACTERISTICS
OF AN 80-DEG SWEPT DELTA WING IN WING ROCK OR FREE YAWING |
ICAS2012-3.1.ST1 |
Liu, G. Z. |
FLOW
CONTROL TEST RESEARCH OF AIRCRAFT MODEL WITH ADJUSTABLE CANAEDS |
ICAS2012-P2.5 |
Liu, H. -Y. |
NUMERICAL STUDY ON RESIDUAL
THERMAL STRESSES IN CARBON FIBRE PULLOUT |
ICAS2012-7.3.1 |
Liu, J. |
COMPARISON OF INFILL
SAMPLING CRITERIA IN KRIGING-BASED AERODYNAMIC OPTIMIZATION |
ICAS2012-11.10.ST |
Liu, J. |
DESIGN OF LAMINAR
SUPERCRITICAL AIRFOILS BASED ON NAVIER-STOKES EQUATIONS |
ICAS2012-2.2.2 |
Liu, J. |
LAMINAR FLOW WING’S
OPTIMIZATION DESIGN BY RANS SOLVER WITH AUTOMATIC TRANSITION PREDICTION |
ICAS2012-2.2.3 |
Liu, L. |
THE
NUMERICAL SIMULATION OF BIRD STRIKE ON BLADES OF AN ENGINE |
ICAS2012-4.4.3 |
Liu, Q. |
MICROSTRUCTURE AND
MECHANICAL PROPERTIES OF LASER CLADDING REPAIR OF AISI 4340 STEEL |
ICAS2012-12.4.4 |
Liu, W. |
STUDY ON THE FLOW STRUCTURES
OF THE SHOCKWAVE AND TURBULENT BOUNDARY-LAYER INTERACTION |
ICAS2012-11.4.3 |
Liu, Y. |
CONTROL ALLOCATION FOR
AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS DURING TAKEOFF AND LANDING PHASES |
ICAS2012-5.3.3 |
Loader, C. |
INITIAL RESULTS FROM DSTO’S
CORROSION STRUCTURAL INTEGRITY ROADMAP |
ICAS2012-12.6.1 |
Lobentanzer, H. |
VOLTAIR - THE ALL ELECTRIC
PROPULSION CONCEPT PLATFORM – A VISION FOR ATMOSPHERIC FRIENDLY FLIGHT |
ICAS2012-4.7.2 |
Lööf, J. |
ROBUST LIFECYCLE
OPTIMIZATION OF TURBINE COMPONENTS USING SIMULATION PLATFORMS |
ICAS2012-4.3.2 |
Lorenz, L. |
PROGRESS AND PERSPECTIVES OF
ELECTRIC AIR TRANSPORT |
ICAS2012-8.6.1 |
Loth, S. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
Love, J. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
Lowe, A. |
A METHOD FOR THE EVALUATION
OF ELECTROMECHANICAL ACTUATOR SYSTEMS USING EXERGY |
ICAS2012-6.6.3 |
Lowenberg, M. H. |
COMPUTATIONAL AND
EXPERIMENTAL ANALYSIS OF THE ACTIVE MORPHING WING CONCEPT |
ICAS2012-2.5.3 |
Lu, G. |
THE INTEGRATION METHOD OF
FAULT DIAGNOSIS AND HEALTH ASSESSMENT FOR UAV SYSTEM |
ICAS2012-12.1.3 |
Lu, H. Y. |
STUDY OF THE PRESSURE DROP
FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
ICAS2012-4.4.ST |
Lu, Y. L |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
Luber, W. G. |
AEROSERVOELASTIC FLIGHT CONTROL DESIGN FOR A MILITARY COMBAT AIRCRAFT WEAPON SYSTEM |
ICAS2012-5.4.2 |
Lucchi, F. |
INNOVATION IN MAN MACHINE
INTERFACES: USE OF 3D CONFORMAL SYMBOLS IN THE DESIGN OF FUTURE HUDS (HEAD UP
DISPLAYS) |
ICAS2012-9.7.2 |
Lukovnikov, A. V. |
STUDIES
OF PROPULSION SYSTEM CONCEPTS FOR ADVANCED SUBSONIC AIRLINERS |
ICAS2012-4.7.3 |
Lukyanov, A. V. |
DEVELOPMENT OF THE AUTOMATED
SYSTEM ON THE BASIS OF NEURAL NETWORKS FOR FLIGHT SAFETY OF AIRCRAFT |
ICAS2012-5.2.2 |
Lunsdström, D. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
Luo, X. |
STUDY OF THE PRESSURE DROP
FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
ICAS2012-4.4.ST |
Lwin, T. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
Lyubimov, D. |
EXPERIMENTAL AND NUMERICAL
RESEARCH OF UNSTEADY FLOW IN CURVILINEAR CHANNEL WITH ACTIVE FLOW MANAGEMENT
USING “SYNTHETIC” JETS |
ICAS2012-4.4.2 |
Ma, J. G. |
RESEARCH ON AIRBORNE
INTELLIGENT HYDRAULIC PUMP SYSTEM |
ICAS2012-6.10.3 |
Ma, W. |
A MICRO-SIMULATION OF
AIRPORT PASSENGERS WITH ADVANCED TRAITS |
ICAS2012-10.9.4 |
Ma, Z. |
THE GLARE EVALUATION METHOD
FOR CIVIL AIRPLANE FLIGHT DECK |
ICAS2012-9.3.3 |
Maas, R. |
BUCKLING-OPTIMIZED VARIABLE
STIFFNESS LAMINATES FOR A COMPOSITE FUSELAGE WINDOW SECTION |
ICAS2012-8.9.3 |
Machunze, W. |
DESIGN, ANALYSIS AND
MANUFACTURING OF A THERMOPLASTIC UD CF-PEEK SLAT |
ICAS2012-6.1.1 |
Magerramova, L. |
ACHIEVEMENT OF BIMETALLIC
BLISKS INTEGRATED DISSIMILAR ALLOYS FOR PROMISING HIGH TEMPERATURE AVIATION
GAS TURBINE ENGINES |
ICAS2012-4.1.3 |
Magerramova, L. A. |
INTERDISCIPLINARY COMPLEX
DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES |
ICAS2012-4.3.3 |
Makarov, A. |
EXPERIMENTAL AND NUMERICAL
RESEARCH OF UNSTEADY FLOW IN CURVILINEAR CHANNEL WITH ACTIVE FLOW MANAGEMENT
USING “SYNTHETIC” JETS |
ICAS2012-4.4.2 |
Makaryants, G. M. |
THE INSTABILITY OF THE
PIPELINE DUE TO TRANSPORTING FLUID’S PRESSURE RIPPLES |
ICAS2012-8.11.1 |
Malinin, V. V. |
NUMERICAL MODELING OF FLOW
IN GASDYNAMIC RESONATOR AND MODEL VALIDATION BY RESULTS OF PULSE ENGINE TESTS |
ICAS2012-P4.10 |
Malis, M. |
THE CFRP SAILPLANE WING
SEGMENTS MANUFACTURED BY FILAMENT PLACEMENT |
ICAS2012-7.5.ST |
Malm, A. M. |
MODEL BASED DEFINITION
WITHIN RELOCATION OF AIRCRAFT PRODUCTION |
ICAS2012-9.9.4 |
Mandanis, G. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
Mane, M. |
DESCRIPTION AND EVALUATION
OF MULTI-THREAT TRACKING ARCHITECTURES |
ICAS2012-11.2.3 |
Mangion, D. Z. |
RUNWAY CONFLICT ALERTING
DURING TAKE-OFF AND LANDING: ADVISORY OR DIRECTIVE? |
ICAS2012-9.10.1 |
Maphanga, S. |
A PRACTICAL, ROUTE-BASED
APPROACH TO AIRSPACE CAPACITY MANAGEMENT |
ICAS2012-10.2.2 |
Maqsood, A. |
FLEXIBLE WING AERODYNAMICS
AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.1 |
Maqsood, A. |
EXPERIMENTAL INVESTIGATION
OF A BI-PLANE MICRO AIR VEHICLE |
ICAS2012-3.3.4 |
Marchetti, M. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
Mare, J. -C. |
COUPLING MECH. & THERMAL
MODELS IN PRELIMINARY DESIGN OF POWER TRANSMISSIONS DRIVEN BY THERMAL ISSUES |
ICAS2012-6.6.1 |
Mare, J. -C. |
INVESTIGATION IN THE DYNAMIC
FORCE EQUALIZATION OF DISSIMILAR REDUNDANT ACTUATION SYSTEMS OPERATING IN
ACTIVE/ACTIVE MODE |
ICAS2012-6.8.1 |
Marguet, S. |
POSTBUCKLING COMPUTATION OF
LARGE STIFFENED STRUCTURES |
ICAS2012-8.1.3 |
Marino, M. |
THE INFLUENCE OF TURBULENCE
INTENSITY ON THE FLOW STRUCTURE OVER A THIN AIRFOIL AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.2 |
Marino, M. |
OPTIMUM LOCATION OF PRESSURE
MEASUREMENTS AROUND A WING AS A DYNAMIC CONTROL INPUT IN SMOOTH AND TURBULENT
CONDITIONS |
ICAS2012-3.3.3 |
Markwart, M. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
Marques, J. M. G. |
A PROBABILITY ASSESSMENT OF
THE FLIGHT SAFETY RELEVANT TO COLLISION AVOIDANCE |
ICAS2012-10.7.5 |
Marshall, D. D. |
BEYOND TWO-EQUATION
TURBULENCE MODELING FOR THE REYNOLDS-AVERAGED NAVIER-STOKES EQUATIONS:
ADVANCES IN COMPLEX FLOW PREDICTIONS |
ICAS2012-2.4.1 |
Marta, A. C. |
ANALYTICAL NATURAL
FREQUENCIES OF TAPERED WINGS |
ICAS2012-P3.2 |
Martensson, H. |
CFD OPTIMIZATION OF A
TRANSONIC COMPRESSOR USING MULTIOBJECTIVE GA AND METAMODELS |
ICAS2012-4.6.3 |
Martin, E. L. |
DEVELOPMENT OF AN
EXPERIMENTAL TECHNIQUE FOR HIGH TEMPERATURE IMPINGEMENT STUDIES |
ICAS2012-12.6.3 |
Martin, L. |
RESOLVING OFF-NOMINAL
SITUATIONS IN SCHEDULE-BASED TERMINAL AREA OPERATIONS: RESULTS FROM A
HUMAN-IN-THE-LOOP SIMULATION |
ICAS2012-10.5.2 |
Martinez, G. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
Martínez, M. |
PRELIMINARY AERODYNAMIC
INVESTIGATION OF AN UNMANNED BOX-WING AIRCRAFT |
ICAS2012-P2.13 |
Martínez-Val, R. |
CARRIER SUITABILITY OF
LAND-BASED AIRCRAFT |
ICAS2012-1.1.ST |
Mason, M. |
THE AFFECT OF SCREEN SIZE ON
MISSION COMMANDER’S SITUATION AWARENESS |
ICAS2012-9.7.5 |
Masson, B. |
ENGINE-OUT TAKEOFF PATH
OPTIMIZATION OUT OF TERRAIN CHALLENGING AIRPORTS |
ICAS2012-5.8.2 |
Masuya, G. |
EFFECT OF VENT MIXER TO
MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
ICAS2012-P4.4 |
Mateescu, D. |
STEADY
AND UNSTEADY FLOWS PAST AIRFOILS AT LOW REYNOLDS NUMBERS IN THE PROXIMITY OF
THE GROUND |
ICAS2012-3.6.ST |
Mateják, V. |
THE DETERMINATION OF
DELAMINATION STRAIN ENERGY RELEASE RATE OF COMPOSITE BI-MATERIAL INTERFACE |
ICAS2012-7.4.1 |
Matsuda, Y. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
Matsuno, T. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
Matsuo, Y. |
NUMERICAL STUDY OF THE
EFFECTS OF CROSS-WIND ON THE JET BLAST DEFORMATION |
ICAS2012-10.10.3 |
Matsushima, K. |
DEVELOPMENT OF SUPERSONIC
NATURAL LAMINAR FLOW WING DESIGN SYSTEM USING CFD-BASED INVERSE METHOD |
ICAS2012-2.2.1 |
Matthews, N. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
Mavris, D. |
STATISTICAL STABILITY AND
CONTROL ANALYSIS TO INVESTIGATE THE CONTROL EFFORT OF IMPROVING HANDLING
QUALITY CHARACTERISTICS |
ICAS2012-5.9.1 |
Mavris, D. |
A METHOD FOR THE EVALUATION
OF ELECTROMECHANICAL ACTUATOR SYSTEMS USING EXERGY |
ICAS2012-6.6.3 |
Mavris, D. |
DESIGN OF UNMANNED AIR
SYSTEMS FOR USE IN SEARCH AND RESCUE IN THE NORTH ATLANTIC |
ICAS2012-9.9.3 |
Mavris, D. N. |
A COMPETITIVE AND
REAL-OPTIONS FRAMEWORK FOR THE ECONOMIC ANALYSIS OF LARGE AEROSPACE PROGRAMS |
ICAS2012-6.3.2 |
Mavris, D. N. |
A NON-WEIGHT BASED,
MANUFACTURING INFLUENCED DESIGN (MIND) METHODOLOGY FOR PRELIMINARY DESIGN |
ICAS2012-6.4.3 |
Mavris, D. N. |
A METHODOLOGY FOR PARAMETRIC
PRODUCTION PLANNING IN PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-6.4.4 |
Mavris, D. N. |
METHODOLOGY FOR THE DESIGN
OF UNMANNED AIRCRAFT PRODUCT FAMILIES |
ICAS2012-9.9.2 |
Mavris, D. N. |
EVALUATING FLEXIBILITY IN
AIRPORT CAPACITY-ENHANCING TECHNOLOGY INVESTMENTS |
ICAS2012-P8.2 |
Maximov, A. A. |
STUDIES
OF PROPULSION SYSTEM CONCEPTS FOR ADVANCED SUBSONIC AIRLINERS |
ICAS2012-4.7.3 |
Mayes, P. |
EFFECTIVE SAFETY MANAGEMENT
SYSTEMS FOR ACCIDENT PREVENTION |
ICAS2012-9.10.2 |
McCann, H. M. |
VIBRATION AND AEROELASTIC CLEARANCE WORK FOR JASSM INTEGRATION ONTO THE F/A-18A/B |
ICAS2012-8.10.3 |
McCarthy, J. M. |
FLOW-INDUCED FLUTTER OF
SLENDER CANTILEVER HIGH-COMPLIANCE PLATES |
ICAS2012-8.10.5 |
McDonald, M. |
QUANTITATIVE FRACTOGRAPHY
MARKERS FOR DETERMINING FATIGUE CRACK GROWTH RATES IN ALUMINIUM AND TITANIUM
AIRCRAFT STRUCTURES |
ICAS2012-12.4.1 |
Mcfadyen, A. D. |
VISUAL SERVOING APPROACH TO
COLLISION AVOIDANCE FOR AIRCRAFT |
ICAS2012-11.3.1 |
McIntyre, T. J. |
STUDY OF RADIATIVE HEAT
TRANSFER IN TITAN ATMOSPHERIC ENTRY |
ICAS2012-3.8.3 |
McLeod, J. E. |
BI-AXIAL VIBRATION ENERGY
HARVESTING FOR USE ON AEROSPACE PLATFORMS |
ICAS2012-6.7.1 |
McMullan, W. A. |
STREAMWISE AND CROSSFLOW
INSTABILITIES ON INCLINED CIRCULAR CYLINDERS |
ICAS2012-3.10.2 |
McNally, D. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
Medford, C. M. |
WATER TUNNEL FORCE AND
MOMENT STUDIES OF A MANEUVERING UCAV 1303 AND THEIR CONTROL |
ICAS2012-3.1.3 |
Medici, G. |
INTEROPERABILITY OF MILITARY
AIRCRAFT VERSUS FUTURE AIR NAVIGATION SYSTEM (FANS) |
ICAS2012-10.1.3 |
Medici, G. |
TURBOJET ANALYTICAL MODEL
DEVELOPMENT AND VALIDATION |
ICAS2012-4.10.5 |
Mejias, L. |
FLIGHT TRIAL OF AN
ELECTRO-OPTICAL SENSE-AND-AVOID SYSTEM |
ICAS2012-11.2.1 |
Mejias, L. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
Mejias, L. A. |
VISUAL SERVOING APPROACH TO
COLLISION AVOIDANCE FOR AIRCRAFT |
ICAS2012-11.3.1 |
Melin, T. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
Melin, T. |
DESIGN OF UNMANNED AIR
SYSTEMS FOR USE IN SEARCH AND RESCUE IN THE NORTH ATLANTIC |
ICAS2012-9.9.3 |
Meng, P. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
Mercer, J. |
RESOLVING OFF-NOMINAL
SITUATIONS IN SCHEDULE-BASED TERMINAL AREA OPERATIONS: RESULTS FROM A
HUMAN-IN-THE-LOOP SIMULATION |
ICAS2012-10.5.2 |
Metkemeijer, R. |
APACHE : INTEGRATED HYBRID
FUEL CELL SYSTEM FOR 2-SEAT ALL ELECTRIC AIRCRAFTS PROPULSION |
ICAS2012-6.7.4 |
Micallef, M. |
A PROPOSAL FOR REVISED
APPROACHES AND PROCEDURES TO MALTA INTERNATIONAL AIRPORT |
ICAS2012-4.9.3 |
Mieloszyk, J. |
MADO – SOFTWARE PACKAGE FOR
HIGH ORDER MULTIDISCIPLINARY AIRCRAFT
DESIGN AND OPTIMIZATION |
ICAS2012-1.9.4 |
Mieloszyk, J. |
RESULTS OF THE GUST
RESISTANT MAV PROGRAMME |
ICAS2012-3.1.1 |
Mieszalski, D. |
MADO – SOFTWARE PACKAGE FOR
HIGH ORDER MULTIDISCIPLINARY AIRCRAFT
DESIGN AND OPTIMIZATION |
ICAS2012-1.9.4 |
Mikhaylov, S. V. |
AN EXPERIENCE OF USING
NUMERICAL METHODS IN EXPERIMENTAL INVESTIGATIONS OF TsAGI |
ICAS2012-P2.6 |
Miki, H. |
PERFORMANCE EVALUATION OF A
BOUNDARY-LAYER DIVERTER FOR SUPERSONIC PROPULSION SYSTEM |
ICAS2012-6.2.2 |
Milanese, A. |
EXPERIMENTAL AND NUMERICAL
ASSESSMENT OF HELICOPTER SUBFLOOR CRASHWORTHINESS |
ICAS2012-8.1.1 |
Milanese, A. |
PRELIMINARY INVESTIGATION ON
THE FEASIBILITY OF A BIRD SURROGATE FOR FULL-SCALE BIRD IMPACT TEST |
ICAS2012-8.3.1 |
Mileshin, V. |
STUDY ON NOISE OF COUNTER
ROTATING FAN MODELS AT CIAM ANECHOIC CHAMBER |
ICAS2012-3.9.4 |
Mileshin, V. I. |
EXPERIMENTAL AND NUMERICAL
STUDY OF TWO FIRST HIGHLY-LOADED STAGES OF COMPRESSORS AS A PART OF HPC AND
SEPARATE UNIT |
ICAS2012-4.6.1 |
Minaeifard, F. |
AN
OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES |
ICAS2012-6.5.ST |
Minami, Y. |
AUTOPILOT
DESIGN FOR THE EOLE DEMONSTRATOR |
ICAS2012-5.3.4 |
Minato, R. |
DEVELOPMENT OF A SMALL-SCALE
SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED |
ICAS2012-1.2.2 |
Mirkov, N. |
MANEUVERABILITY OF AN UAV
WITH COANDA EFFECT BASED LIFT PRODUCTION |
ICAS2012-P2.18 |
Mirzaei, M. |
AN
OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES |
ICAS2012-6.5.ST |
Mirzoyan, A. |
STUDIES ON REQUIRED
PERFORMANCES OF ADVANCED SUPERSONIC CIVIL AIRCRAFT AND THEIR PROPULSION
SYSTEMS FOR 2020-2035 TIMEFRAME |
ICAS2012-4.7.4 |
Mirzoyan, L. |
STUDIES ON REQUIRED
PERFORMANCES OF ADVANCED SUPERSONIC CIVIL AIRCRAFT AND THEIR PROPULSION
SYSTEMS FOR 2020-2035 TIMEFRAME |
ICAS2012-4.7.4 |
Mitchell, T. M. |
ENHANCING THE "LAST
MILE" COMMUNICATIONS AT AIRPORTS |
ICAS2012-10.10.5 |
Miura, T. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
Miyaji, K. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
Miyatsu, Y. |
A BASIC STUDY ON EFFICIENCY IN JAPANESE
AIRSPACE |
ICAS2012-10.2.1 |
Miyazato, Y. |
THEORETICAL AND EXPERIMENTAL
INVESTIGATIONS ON CHOKING PHENOMENA OF AXISYMMETRIC CONVERGENT NOZZLE FLOW |
ICAS2012-P2.11 |
Miyazawa, Y. |
FLIGHT TRAJECTORY
OPTIMIZATION FOR AN EFFICIENT AIR TRANSPORTATION SYSTEM |
ICAS2012-5.8.3 |
Mizobata, K. |
DEVELOPMENT OF A SMALL-SCALE
SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED |
ICAS2012-1.2.2 |
Mizukaki, T. |
INSTABILITY CHARACTERISTICS
OF SHOCK WAVES AHEAD OF A HEMISPHERICAL SHELL AT SUPERSONIC SPEEDS |
ICAS2012-11.4.2 |
Mizukaki, T. |
VISUALIZATION OF UNSTEADY
BEHAVIOR OF SHOCK WAVES AROUND SUPERSONIC INTAKE INSTALLED IN SHOCK TUNNEL |
ICAS2012-P4.5 |
Mohammadi-Amin, M. |
NONLINEAR AEROELASTIC
ANALYSIS OF SWEPT WINGS IN COMPRESSIBLE FLOW VIA THE HARMONIC BALANCE METHOD |
ICAS2012-8.7.1 |
Mohseni Shakib, S. M. |
POST-BUCKLING
BEHAVIOR AND PROPAGATION OF DELAMINATION FOR COMPOSITE PANELS IN DIFFERENT
DELAMINATION SIZES |
ICAS2012-7.9.ST |
Mohseni Shakib, S. M. |
BUCKLING
AND POST-BUCKLING RESPONSES OF SQUARE LAMINATE WITH VARIOUS SHAPED CUTOUTS
UNDER DIFFERENT LOADINGS |
ICAS2012-P3.7 |
Molent, L. |
INVESTIGATION OF AN
IN-SERVICE CRACK SUBJECTED TO AERODYNAMIC BUFFET AND MANOEUVRE LOADS AND
EXPOSED TO AN CORROSIVE ENVIRONMENT |
ICAS2012-7.9.1 |
Mollaei, F. |
FINDING TUNING FREQUENCY OF
SYMMETRIC AND ANTI-SYMMETRIC LAMB WAVES USING FEM |
ICAS2012-P3.6 |
Mollwitz, V. |
FLIGHT TESTING OF NOISE
ABATING RNP PROCEDURES AND STEEP APPROACHES |
ICAS2012-4.9.1 |
Momeni Massouleh, S. H. |
APPLICATION
OF SINGULAR VALUE DECOMPOSITION IN COMPONENT MODE SYNTHESIS WITH EXPERIMENTAL
APPROACH |
ICAS2012-8.11.3 |
Montrucchio, C. |
INTEROPERABILITY OF MILITARY
AIRCRAFT VERSUS FUTURE AIR NAVIGATION SYSTEM (FANS) |
ICAS2012-10.1.3 |
Mooij, M. |
A CAPABILITY FRAMEWORK FOR
MULTIPLE HETEROGENEOUS UAVS: FROM A MISSION COMMANDER'S PERSPECTIVE |
ICAS2012-9.7.3 |
Moolchandani, K. A. |
DEVELOPING OPTIMAL AIRLINE
FLEETS UNDER ENVIRONMENTAL AND CAPACITY CONSTRAINTS |
ICAS2012-7.10.1 |
Moormann, D. |
MODEL VALIDATION OF A
TILTWING UAV IN TRANSITION PHASE APPLYING WINDTUNNEL INVESTIGATIONS |
ICAS2012-11.1.1 |
Moormann, D. |
CONTROL CONCEPT OF A
TILTWING UAV DURING LOW SPEED MANOEUVRING |
ICAS2012-11.1.2 |
Moosavi, M. R. |
FINDING TUNING FREQUENCY OF
SYMMETRIC AND ANTI-SYMMETRIC LAMB WAVES USING FEM |
ICAS2012-P3.6 |
Moreau, D. J. |
EXPERIMENTAL INVESTIGATION
OF FLAT PLATE SELF-NOISE REDUCTION USING TRAILING EDGE SERRATIONS |
ICAS2012-9.11.1 |
Moreau, S. |
MULTI-OBJECTIVE OPTIMIZATION
OF MULTI-ELEMENT HIGH-LIFT AIRFOIL |
ICAS2012-2.3.4 |
Moreau, S. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
Moretti, G. |
PRELIMINARY INVESTIGATION ON
THE FEASIBILITY OF A BIRD SURROGATE FOR FULL-SCALE BIRD IMPACT TEST |
ICAS2012-8.3.1 |
Morgan, R. G. |
STUDY OF RADIATIVE HEAT
TRANSFER IN TITAN ATMOSPHERIC ENTRY |
ICAS2012-3.8.3 |
Mori, R. |
AIRCRAFT TAXIING MODEL AT
CONGESTED AIRPORTS |
ICAS2012-10.9.1 |
Morinière, F. D. |
ENERGY DISTRIBUTION IN GLARE
AND 2024-T3 ALUMINIUM DURING LOW-VELOCITY IMPACT |
ICAS2012-7.7.2 |
Mosharov, V. E. |
EXPERIMENTAL AND NUMERICAL
INVESTIGATIONS OF LOCAL AERODYNAMICS OF CIVIL AIRCRAFT |
ICAS2012-2.9.4 |
Moss, S. D. |
BI-AXIAL VIBRATION ENERGY
HARVESTING FOR USE ON AEROSPACE PLATFORMS |
ICAS2012-6.7.1 |
Mouritz, A. P. |
DAMAGE TOLERANCE OF Z-PINNED
COMPOSITE JOINTS |
ICAS2012-7.5.2 |
Mouritz, A. P. |
DELAMINATION TOUGHENING OF
CARBON-EPOXY LAMINATE WITH A POLYETHYLENE-CO-METHACRYLIC ACID (EMAA)
SELF-HEALING MODIFIER |
ICAS2012-7.6.2 |
Mouser, C. R. |
VIBRATION AND AEROELASTIC CLEARANCE WORK FOR JASSM INTEGRATION ONTO THE F/A-18A/B |
ICAS2012-8.10.3 |
Mozzillo, R. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
Mugrauer, R. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
Muhammad, H. |
DEVELOPMENT OF POSE
ESTIMATION SYSTEM BASED ON DUAL CAMERA TECHNIQUES FOR PARAMETER
IDENTIFICATION OF INDOOR MAV |
ICAS2012-11.9.4 |
Mulyanto, T. |
DEVELOPMENT OF POSE
ESTIMATION SYSTEM BASED ON DUAL CAMERA TECHNIQUES FOR PARAMETER
IDENTIFICATION OF INDOOR MAV |
ICAS2012-11.9.4 |
Mumaw, R. |
UNRELIABLE AIRSPEED – MAKING
VALID ASSUMPTIONS ON FLIGHT CREW PERFORMANCE |
ICAS2012-9.3.4 |
Mundt, C. |
IMPROVED MODELLING OF
VORTICAL MIXING FOR THE SIMULATION OF EFFICIENT PROPULSION SYSTEMS |
ICAS2012-4.10.1 |
Munoz, C. |
CONCEPT OF INTEGRATION FOR
UAS OPERATIONS IN THE NAS |
ICAS2012-10.7.1 |
Murakami, K. |
AUTOMATIC HANDLING OF
DEFECTIVE SURFACE GEOMETRY WITHIN GRID GENERATION FOR NAVIER-STOKES
COMPUTATION |
ICAS2012-2.11.1 |
Murakami, K. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
Muraoka, K. |
TRANSITION FLIGHT OF QUAD
TILT WING VTOL UAV |
ICAS2012-11.1.3 |
Muraoka, K. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
Murayama, M. |
COMPUTATIONAL STUDY ON NOISE
GENERATION FROM A TWO-WHEEL MAIN LANDING GEAR |
ICAS2012-3.9.3 |
Murozono, M. |
INVESTIGATION ON STRUCTURAL
AND AERODYNAMIC CHARACTERISTICS OF RESONANT TYPE ELASTIC FLAPPING WING |
ICAS2012-9.5.3 |
Murphy, M. |
ICAO’S BALANCED APPROACH TO
NOISE MANAGEMENT AND ITS INFLUENCE ON THE ECONOMIC IMPACT OF AIR
TRANSPORTATION |
ICAS2012-7.10.4 |
Muscat, A. |
A PROPOSAL FOR REVISED
APPROACHES AND PROCEDURES TO MALTA INTERNATIONAL AIRPORT |
ICAS2012-4.9.3 |
Nagai, H. |
INVESTIGATION ON STRUCTURAL
AND AERODYNAMIC CHARACTERISTICS OF RESONANT TYPE ELASTIC FLAPPING WING |
ICAS2012-9.5.3 |
Nagarathinam, A. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
Nagel, B. |
A KNOWLEDGE BASED APPROACH
FOR EXTENDED PHYSICS-BASED WING MASS ESTIMATION IN EARLY DESIGN STAGES |
ICAS2012-1.1.1 |
Nagel, B. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
Naghipour, P. |
NUMERICAL SIMULATIONS AND
EXPERIMENTAL INVESTIGATIONS ON QUASI-STATIC AND CYCLIC MIXED MODE
DELAMINATION OF MULTIDIRECTIONAL CFRP LAMINATES |
ICAS2012-7.4.2 |
Nagy, A. |
MEASURING AND MODELLING THE
LONGITUDINAL MOTION OF PARAGLIDERS |
ICAS2012-5.10.2 |
Nagy, A. |
UNMANNED MEASUREMENT
PLATFORM FOR PARAGLIDERS |
ICAS2012-P1.4 |
Nakamura, H. |
SCIENCE AND TECHNOLOGY MAP
ANALYSIS OF AEROSPACE ENGINEERING |
ICAS2012-P7.1 |
Nakamura, T. |
DEVELOPMENT OF LAPTOP PC
TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |
ICAS2012-9.10.ST |
Nakamura, Y. |
FUNDAMENTAL CHARACTERISTICS
OF DECENTRALIZED AIR TRAFFIC FLOW CONTROL IN HIGH DENSITY CORRIDOR |
ICAS2012-10.7.2 |
Nakata, N. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
Nakatsuka, S. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
Nam, H. J. |
MODELING OF NO AND OH
INFRARED RADIATION ON A CONVERGENT-DIVERGENT NOZZLE |
ICAS2012-P4.6 |
Naruoka, M. |
REAL-TIME WAVELET FLIGHT
DATA EVALUATOR FOR SYSTEM IDENTIFICATION OF FLIGHT CHARACTERISTICS |
ICAS2012-5.10.4 |
Naruoka, M. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
Nayko, Y. |
AEROELASTIC
MULTIDISCIPLINARY ANALYSIS OF THE FIN
WITH INNOVATIVE ADAPTIVE CONTROL |
ICAS2012-8.7.4 |
Neely, A. J. |
PROGRESS IN UNDERSTANDING
TRANSONIC AND SUPERSONIC GROUND EFFECT AERODYNAMICS |
ICAS2012-10.6.3 |
Negishi, E. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
Neilson, S. V. |
INVESTIGATION INTO OPTIMISED
COMPOSITE SCARF REPAIRS WITH PRACTICAL CONSTRAINTS |
ICAS2012-P3.4 |
Nepomnyashchiy, A. D. |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
Neuheuser, T. |
SYSTEM ANALYSIS OF
PROGNOSTICS AND HEALTH MANAGEMENT SYSTEMS FOR FUTURE TRANSPORT AIRCRAFT |
ICAS2012-12.3.1 |
Neyland, V. Y. |
AN EXPERIENCE OF USING
NUMERICAL METHODS IN EXPERIMENTAL INVESTIGATIONS OF TsAGI |
ICAS2012-P2.6 |
Ng, H. K. |
UNCERTAINTY QUANTIFICATION
IN THE DEVELOPMENT OF AVIATION OPERATIONS TO REDUCE AVIATION EMISSIONS AND
CONTRAILS |
ICAS2012-7.10.2 |
Nguyen-Bui, N. T.-H. |
MODELING OF THE INTERACTION
BETWEEN A TURBULENT FLOW AND AN ABLATABLE MATERIAL |
ICAS2012-3.8.2 |
Nguyen-Bui, T.-H. |
SIMULATION OF THE FULL
COUPLING BETWEEN THE RADIATION TRANSFER AND THE AERODYNAMICS FOR HYPERSONIC REENTRY PROBES |
ICAS2012-3.8.ST |
Nicholson, K. J. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
Nicholson, R. |
UNRELIABLE AIRSPEED – MAKING
VALID ASSUMPTIONS ON FLIGHT CREW PERFORMANCE |
ICAS2012-9.3.4 |
Nicholson, R. K. |
CATEGORIZATION OF UNRELIABLE
AIRSPEED EVENTS USING RASMUSSEN’S HUMAN PERFORMANCE MODEL |
ICAS2012-9.4.4 |
Nicke, E. |
STUDY ON NOISE OF COUNTER
ROTATING FAN MODELS AT CIAM ANECHOIC CHAMBER |
ICAS2012-3.9.4 |
Nicolosi, F. |
AERODYNAMIC ANALYSIS AND
DESIGN OF A TWIN-ENGINE COMMUTER
AIRCRAFT |
ICAS2012-1.6.2 |
Niedermeier, D. |
FLY-BY-WIRE AUGMENTED MANUAL
CONTROL - BASIC DESIGN CONSIDERATIONS |
ICAS2012-5.4.1 |
Niehuis, R. |
NUMERICAL INVESTIGATION OF
THE EFFECT OF INFLOW DISTORTIONS ON TRANSONIC AXIAL COMPRESSOR STAGES WITH 2D
AND 3D CALCULATIONS |
ICAS2012-4.6.2 |
Nieuwenhuisen, D. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
Nieuwenhuisen, D. |
OPTIMIZING INBOUND AIRCRAFT
STREAMS USING AIRCRAFT DERIVED DATA AND RTA FUNCTIONALITY |
ICAS2012-10.4.4 |
Nigmatullin, R. Z. |
INTERDISCIPLINARY COMPLEX
DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES |
ICAS2012-4.3.3 |
Ninomiya, T. |
GUIDANCE AND CONTROL LAW FOR
D-SEND#2 |
ICAS2012-5.3.1 |
Nitsche, W. |
ACTIVE
SEPARATION CONTROL ON A 2D HIGH-LIFT WING SECTION TOWARDS HIGH REYNOLDS
NUMBER APPLICATION |
ICAS2012-3.5.3 |
Nooij, S. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
Noori, B. |
AN
APPROXIMATE ENGINEERING METHOD FOR AERODYNAMIC HEATING SOLUTION AROUND BLUNT
BODY NOES |
ICAS2012-11.4.4 |
Nordin, P. |
AIRCRAFT SYSTEM SIMULATION
FOR PRELIMINARY DESIGN |
ICAS2012-1.9.3 |
Nouri, Z. |
AN
OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES |
ICAS2012-6.5.ST |
Nozhnitskiy, Y. A. |
VIBRATION STRENGTH INCREASE
OF ROTATING BLADES USING DYNAMIC SPIN RIGS |
ICAS2012-12.6.4 |
Nozhnitskiy, Y. A. |
PREVENTION OF LOW CYCLE
FATIGUE FRACTURE OF AVIATION ENGINE CRITICAL PARTS |
ICAS2012-4.1.2 |
Numata, D. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
Nunes, N. |
ASSESSING
HELICOPTER SURVIVABILITY TO GROUND LAUNCHED PROJECTILES USING MULTI-FIDELITY
INVERSE SIMULATION |
ICAS2012-1.4.4 |
Nurhakim, M. L. I. |
DEVELOPMENT OF POSE
ESTIMATION SYSTEM BASED ON DUAL CAMERA TECHNIQUES FOR PARAMETER
IDENTIFICATION OF INDOOR MAV |
ICAS2012-11.9.4 |
O’Byrne, S. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
Ogawa, H. |
ROBUST DESIGN OPTIMIZATION
OF HIGH-PERFORMANCE AXISYMMETRIC SCRAMJETS BASED ON SURROGATE-ASSISTED
EVOLUTIONARY ALGORITHMS |
ICAS2012-4.11.3 |
Oh, H. -U. |
VERIFICATION OF OPTICAL
PAYLOAD CFRP STRUCTURE FOR SATELLITE THROUGH ANALYSIS AND SPACE QUALIFICATION
TEST |
ICAS2012-P3.9 |
Ohira, K. |
NUMERICAL STUDY OF THE
REYNOLDS NUMBER EFFECT ON LOW ASPECT
RATIO WINGS AT LOW SPEED |
ICAS2012-2.10.2 |
Ohira, K. |
DEVELOPMENT OF SUPERSONIC
NATURAL LAMINAR FLOW WING DESIGN SYSTEM USING CFD-BASED INVERSE METHOD |
ICAS2012-2.2.1 |
Ohnuki, T. |
JAXA’S ENVIRONMENT CONSCIOUS
AIRCRAFT TECHNOLOGY PROGRAM PLAN |
ICAS2012-7.11.3 |
Oh-Ohara, S. |
ESTIMATION OF AERODYNAMIC
DERIVATIVES IN AIRCRAFT MODEL USING ITERATIVE LEARNING IDENTIFICATION |
ICAS2012-5.10.5 |
Ohsawa, R. |
DEVELOPMENT OF OBSERVATIONAL
SYSTEM WITH UNMANNED FLIGHT SYSTEM |
ICAS2012-P5.10 |
Ohta, K. |
GUST RESPONSE ANALYSIS IN
THE FLIGHT FORMATION OF UNMANNED AIR VEHICLES |
ICAS2012-P5.9 |
Okada, N. |
TRANSITION FLIGHT OF QUAD
TILT WING VTOL UAV |
ICAS2012-11.1.3 |
Okumura, K. |
THE FLAPPING AIRCRAFT
DYNAMICS WITH WING DEFORMATION UNDER GUST INPUT |
ICAS2012-11.9.2 |
Olbrechts, T. |
DESIGN STUDY OF AN ACTIVE
GURNEY FLAP SYSTEM FOR HELICOPTER ROTOR BLADES |
ICAS2012-6.11.1 |
Olbrechts, T. |
IDENTIFICATION OF HELICOPTER
GROUND RESONANCE WITH MULTI-BODY SIMULATION |
ICAS2012-8.3.2 |
Olbrechts, T. |
RELIABILITY ANALYSIS OF
AIRCRAFT SYSTEM ARCHITECTURES |
ICAS2012-P9.1 |
Olsen, J. F. |
INFORMATION THEORY APPLIED
TO A SELF-ORGANISED, UNMANNED AERIAL SYSTEM |
ICAS2012-11.7.4 |
Omer, J. |
AUTOMATED CONFLICT-FREE
PLANNING: EXPERIMENTS ON REAL AIR TRAFFIC DATA |
ICAS2012-10.1.2 |
Onate, E. |
ROBUST AERODYNAMIC DESIGN
OPTIMISATION OF MORPHING AEROFOIL/WING USING DISTRIBUTED MOGA |
ICAS2012-11.10.3 |
Ono, D. |
THEORETICAL AND EXPERIMENTAL
INVESTIGATIONS ON CHOKING PHENOMENA OF AXISYMMETRIC CONVERGENT NOZZLE FLOW |
ICAS2012-P2.11 |
Orekhov, I. K. |
EXPERIMENTAL AND NUMERICAL
STUDY OF TWO FIRST HIGHLY-LOADED STAGES OF COMPRESSORS AS A PART OF HPC AND
SEPARATE UNIT |
ICAS2012-4.6.1 |
Oreschko, B. |
DYNAMIC TURNAROUND
MANAGEMENT IN A HIGHLY AUTOMATED AIRPORT ENVIRONMENT |
ICAS2012-10.9.2 |
Orifici, A. C. |
CRITICAL ASSESSMENT OF
FAILURE CRITERION FOR ADHESIVELY BONDED COMPOSITE JOINT REPAIR DESIGN |
ICAS2012-12.2.2 |
Orifici, A. C. |
INVESTIGATION INTO OPTIMISED
COMPOSITE SCARF REPAIRS WITH PRACTICAL CONSTRAINTS |
ICAS2012-P3.4 |
O'Shea, P. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
Ostermann, T. |
MODEL VALIDATION OF A
TILTWING UAV IN TRANSITION PHASE APPLYING WINDTUNNEL INVESTIGATIONS |
ICAS2012-11.1.1 |
Ostermann, T. |
CONTROL CONCEPT OF A
TILTWING UAV DURING LOW SPEED MANOEUVRING |
ICAS2012-11.1.2 |
Oswald, J. J. |
EOLE, AN INNOVATIVE FLYING
SCALE DEMONSTRATOR FOR AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS |
ICAS2012-1.11.2 |
Öttl, G. |
A SCENARIO-BASED APPROACH TO
DEVELOP REPRESENTATIVE TRAFFIC ENVIRONMENTS FOR OPERATIONAL AIRCRAFT
EVALUATION |
ICAS2012-6.3.1 |
Ozerciyes, V. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
Paces, P. |
ADVANCED DISPLAY AND
POSITION ANGLES MEASUREMENT SYSTEMS |
ICAS2012-P6.3 |
Pacino, M. |
VERY-LONG ENDURANCE SOLAR
POWERED AUTONOMOUS UAVS: ROLE AND CONSTRAINTS FOR GMES APPLICATIONS |
ICAS2012-4.7.5 |
Page, J. |
ENGINE-OUT TAKEOFF PATH
OPTIMIZATION OUT OF TERRAIN CHALLENGING AIRPORTS |
ICAS2012-5.8.2 |
Page, J. R. |
INFORMATION THEORY APPLIED
TO A SELF-ORGANISED, UNMANNED AERIAL SYSTEM |
ICAS2012-11.7.4 |
Palizvan, M. |
POST-BUCKLING
BEHAVIOR AND PROPAGATION OF DELAMINATION FOR COMPOSITE PANELS IN DIFFERENT
DELAMINATION SIZES |
ICAS2012-7.9.ST |
Palizvan, M. |
BUCKLING
AND POST-BUCKLING RESPONSES OF SQUARE LAMINATE WITH VARIOUS SHAPED CUTOUTS
UNDER DIFFERENT LOADINGS |
ICAS2012-P3.7 |
Palmer, J. L. |
HARDWARE-IN-THE-LOOP
SIMULATION OF FUEL-CELL-BASED HYBRID-ELECTRICAL UAV PROPULSION |
ICAS2012-4.5.2 |
Palmer, J. L. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
Paluch, P. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
Pan, W. |
PATH PLANNING FOR MULTI
HELICOPTER COORDINATED RESCUE |
ICAS2012-P8.5 |
Pankov, A. V. |
FATIGUE DESIGN PROCEDURE OF
LONGITUDINAL AND TRANSVERSE FUSELAGE JOINTS |
ICAS2012-12.4.2 |
Paquet, J. B. |
AEROELASTIC SIMULATION OF
FLEXIBLE FLAPPING WING BASED ON STRUCTURAL FEM AND QUASI-STEADY AERODYNAMIC
MODEL |
ICAS2012-8.5.1 |
Park, J. -W. |
A PEG-BASED ASCENDING
GUIDANCE ALGORITHM FOR RAMJET-POWERED VEHICLES |
ICAS2012-5.7.4 |
Park, J. -W. |
UAV COLLISION AVOIDANCE VIA
OPTIMAL TRAJECTORY GENERATION METHOD |
ICAS2012-P5.5 |
Parker, R. |
HOT END TECHNOLOGY FOR
ADVANCED, LOW EMISSION LARGE CIVIL AIRCRAFT ENGINES |
ICAS2012-4.10.2 |
Patek, Z. |
WIND TUNNEL AND CFD STUDY OF
AIRFOIL WITH AIRBRAKE |
ICAS2012-10.6.ST1 |
Patel, S. |
BOUNDARY LAYER TRANSITION
DETECTION USING TEMPERATURE SENSITIVE PAINT IN THE ARA TRANSONIC WIND TUNNEL |
ICAS2012-3.4.2 |
Paton, R. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
Paull, A. |
HIFIRE: AN INTERNATIONAL COLLABORATION TO ADVANCE THE SCIENCE AND TECHNOLOGY OF HYPERSONIC FLIGHT |
ICAS2012-0.8 |
Pavlenko, A. A. |
THE INVESTIGATION OF A
POSSIBILITY OF INCREASING THE LIFT-TO-DRAG RATIO OF A MANEUVERABLE AIRCRAFT
AT SUBSONIC SPEEDS |
ICAS2012-2.10.3 |
Pearce, G. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
Pearce, G. |
DIRECTIONAL ENHANCEMENT OF
COMPOSITE STRUCTURES ENERGY ABSORPTION USING MAGNETORHEOLOGICAL FLUIDS |
ICAS2012-7.8.1 |
Pearce, G. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
Pearce, G. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
Pechloff, A. |
SMALL DISTURBANCE
NAVIER-STOKES INVESTIGATIONS OF FIGHTER-TYPE-DELTA-WING PITCHING OSCILLATIONS |
ICAS2012-2.11.2 |
Pëna, E. L. |
WEIGHT ON WHEEL SYSTEM BASED
ON STRAIN GAUGES |
ICAS2012-6.11.2 |
Peng, X. B. |
STRUCTURAL
INTEGRITY ANALYSIS AND TEST OF FATIGUE CRITICAL LOCATION OF MA60 REGIONAL JET |
ICAS2012-7.9.4 |
Perdones-Diaz, D. |
CFD BASED AEROELASTIC
CALCULATION OF PROPELLER LOADS |
ICAS2012-9.8.1 |
Perez, T. |
COMPUTATIONAL ASPECTS OF
PROBABILISTIC ASSESSMENT OF UAS ROBUST AUTONOMY |
ICAS2012-9.2.2 |
Perez, T. |
EVALUATION OF ROBUST
AUTONOMY AND IMPLICATIONS ON UAS DESIGN |
ICAS2012-9.4.2 |
Periaux, J. |
ROBUST AERODYNAMIC DESIGN
OPTIMISATION OF MORPHING AEROFOIL/WING USING DISTRIBUTED MOGA |
ICAS2012-11.10.3 |
Perner, M. |
IMPROVING THE PRODUCTION
QUALITY OF THE ADVANCED AUTOMATED FIBER PLACEMENT PROCESS BY MEANS OF ONLINE
PATH CORRECTION |
ICAS2012-6.1.3 |
Persiani, F. |
DESIGN ANALYSIS FOR HYBRID
PROPULSION |
ICAS2012-6.7.5 |
Persiani, F. |
INNOVATION IN MAN MACHINE
INTERFACES: USE OF 3D CONFORMAL SYMBOLS IN THE DESIGN OF FUTURE HUDS (HEAD UP
DISPLAYS) |
ICAS2012-9.7.2 |
Persiani, F. |
A
META-HEURISTIC APPROACH TO SIMULATE TAXI OPERATIONS |
ICAS2012-P8.7 |
Persson, I. |
EXTERNAL AERODYNAMIC
PRESSURE LOADS FOR A RIGID FIGHTER AIRCRAFT, A COMPARISON BETWEEN PSP AND CFD |
ICAS2012-10.6.2 |
Persson, P. |
A COUPLED AERO AND
STRUCTURAL DYNAMICS MODEL FOR COMPUTATION OF UNSTEADY LOADS ON THE HELICOPTER
SKELDAR V200 |
ICAS2012-8.7.2 |
Petersen, P. |
THE INFLUENCE OF TURBULENCE
INTENSITY ON THE FLOW STRUCTURE OVER A THIN AIRFOIL AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.2 |
Petersson, O. |
MULTIDISCIPLINARY AIRFRAME
DESIGN OPTIMIZATION |
ICAS2012-0.4 |
Petrov, A. V. |
AERODYNAMICS OF STOL
AIRPLANES WITH POWERED HIGH-LIFT SYSTEMS |
ICAS2012-9.5.2 |
Pezzella, G. |
AEROTHERMODYNAMIC FIELD PAST
A REENTRY CAPSULE FOR SAMPLE RETURN MISSIONS |
ICAS2012-3.8.1 |
Philippe, M. J. |
A PRACTICAL, ROUTE-BASED
APPROACH TO AIRSPACE CAPACITY MANAGEMENT |
ICAS2012-10.2.2 |
Philit, M. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
Picart, P. |
SUBSONIC WAKE FLOWS ANALYSIS
BY DIGITAL THREE-WAVELENGTHS HOLOGRAPHIC INTERFEROMETRY |
ICAS2012-3.11.3 |
Pickhaver, T. W. |
A TECHNIQUE TO PREDICT THE
AERODYNAMIC LOSSES OF BATTLE DAMAGED WINGS |
ICAS2012-3.2.2 |
Pingkarawat, K. |
DELAMINATION TOUGHENING OF
CARBON-EPOXY LAMINATE WITH A POLYETHYLENE-CO-METHACRYLIC ACID (EMAA)
SELF-HEALING MODIFIER |
ICAS2012-7.6.2 |
Pinna, M. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
Pinon, O. J. |
EVALUATING FLEXIBILITY IN
AIRPORT CAPACITY-ENHANCING TECHNOLOGY INVESTMENTS |
ICAS2012-P8.2 |
Pisarev, V. S. |
INVESTIGATION OF CRACK
PROPAGATION BY OPTICAL INTERFEROMETRIC MEASUREMENTS OF LOCAL DEFORMATION
RESPONSE |
ICAS2012-7.9.2 |
Pistek, A. |
ANALYTICAL METHOD FOR LIMIT
LOAD CAPACITY CALCULATION OF THIN WALLED AIRCRAFT STRUCTURES |
ICAS2012-8.2.ST |
Pitt, S. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
Plokhikh, V. P. |
ADVANCED AEROSPACE SYSTEMS
WITH INTERCONTINENTAL AND GLOBAL RANGE OF FLIGHT |
ICAS2012-1.5.2 |
Plot, S. |
THE ONERA ELSA CFD SOFTWARE
: INPUT FROM RESEARCH AND FEEDBACK FROM INDUSTRY |
ICAS2012-2.1.1 |
Plötner, K. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
Pogaru, S. |
A NON-WEIGHT BASED,
MANUFACTURING INFLUENCED DESIGN (MIND) METHODOLOGY FOR PRELIMINARY DESIGN |
ICAS2012-6.4.3 |
Poirel, D. |
NUMERICAL SIMULATIONS OF
SELF-SUSTAINED AEROELASTIC OSCILLATIONS AT LOW REYNOLDS NUMBERS |
ICAS2012-2.6.3 |
Polikarpov, V. G. |
METHODS AND FACILITIES TO BE
USED TO EVALUATE THE AIRCRAFT FLIGHT AND NAVIGATION EQUIPMENT IN FLIGHT TESTS |
ICAS2012-5.6.3 |
Poovendran, R. |
BALANCING OPERATOR PRIVACY
AND FUTURE AIRSPACE SURVEILLANCE |
ICAS2012-P8.6 |
Popelka, J. |
ADVANCED DISPLAY AND
POSITION ANGLES MEASUREMENT SYSTEMS |
ICAS2012-P6.3 |
Porat, H. |
STUDY OF RADIATIVE HEAT
TRANSFER IN TITAN ATMOSPHERIC ENTRY |
ICAS2012-3.8.3 |
Porretta, M. |
A COMPARISON OF
4D-TRAJECTORY OPERATIONS ENVISIONED FOR 'NEXTGEN' AND 'SESAR', SOME
PRELIMINARY FINDINGS |
ICAS2012-10.3.1 |
Potekhina, I. |
EXPERIMENTAL AND NUMERICAL
RESEARCH OF UNSTEADY FLOW IN CURVILINEAR CHANNEL WITH ACTIVE FLOW MANAGEMENT
USING “SYNTHETIC” JETS |
ICAS2012-4.4.2 |
Pradeepa, T. K. |
TRANSONIC FLUTTER, SHOCKS,
AND PARAMETER EFFECTS |
ICAS2012-2.6.4 |
Premachandran, S. |
NUMERICAL STUDY ON THE
EFFECT OF VARYING SPANWISE TWIST ON LOW-REYNOLDS-NUMBER FLAPPING FLIGHT |
ICAS2012-2.5.1 |
Prince, S. A. |
AN EXPERIMENTAL AND
NUMERICAL STUDY OF THE EFFECT OF NOSE BLUNTING ON A CONICAL NOSED BODY AT
TRANSONIC SPEED |
ICAS2012-2.8.3 |
Prince, S. A. |
A COMPUTATIONAL STUDY OF THE
AERODYNAMICS OF A SPINNING CYLINDER IN CROSSFLOW OF HIGH REYNOLDS NUMBER |
ICAS2012-3.11.2 |
Prince, S. A. |
AN EXPERIMENTAL STUDY OF A
PULSED AIR JET AND AN ACOUSTIC SYNTHETIC JET ON A LOW SPEED TURBULENT
BOUNDARY LAYER |
ICAS2012-3.5.1 |
Prokofiev, A. B. |
THE INSTABILITY OF THE
PIPELINE DUE TO TRANSPORTING FLUID’S PRESSURE RIPPLES |
ICAS2012-8.11.1 |
Prusty, B. G. |
DIRECTIONAL ENHANCEMENT OF
COMPOSITE STRUCTURES ENERGY ABSORPTION USING MAGNETORHEOLOGICAL FLUIDS |
ICAS2012-7.8.1 |
Prusty, B. G. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
Prusty, G. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
Prusty, G. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
Pruter, I. |
FLIGHT PERFORMANCE OF
LIGHTWEIGHT GYROPLANES |
ICAS2012-5.6.2 |
Qi, H. -F. |
THE FABRICATION AND
CHARACTERIZATION OF TiO2 UV DETECTOR |
ICAS2012-7.3.ST |
Qi, H. T |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
Qi, X. |
RESEARCH ON AIRBORNE
INTELLIGENT HYDRAULIC PUMP SYSTEM |
ICAS2012-6.10.3 |
Qian, G. |
THE STUDY ON THE AIRCRAFT
INTEGRATED CHARACTERS WITH DIFFERENT HEIGHT WINGLETS |
ICAS2012-P2.9 |
Qian, G. P. |
THE COMPREHENSIVE STUDY ON
ADVANCED WINGTIP DEVICES IN LARGE CIVIL AIRCRAFT |
ICAS2012-8.8.3 |
Qian, R. Z. |
MULTI-OBJECTIVE AERODYNAMIC
OPTIMIZATION DESIGN OF MULTI-ELEMENT AIRFOIL USING KRIGING MODEL |
ICAS2012-2.3.ST |
Qin, W. |
DEVELOPMENT
OF THE OPTIMIZED APPROACH AND LANDING TRAJECTORY FOR FUTURE AIR TRANSPORT
SYSTEM |
ICAS2012-P8.1 |
Qu, T. |
ON
THE KNEE-POINT PHENOMENON IN COMPOSITE LAMINATES UNDER LOW-VELOCITY IMPACT
AND QUASI-STATIC INDENTATION |
ICAS2012-7.7.ST |
Quaglia, D. |
TOWARDS TRAJECTORY
PREDICTION AND OPTIMISATION FOR ENERGY EFFICIENCY OF AN AIRCRAFT WITH
ELECTRICAL AND HYDRAULIC ACTUATION SYSTEMS |
ICAS2012-6.7.3 |
Quagliotti, F. |
AN INNOVATIVE MISSION
MANAGEMENT SYSTEM FOR FIXED-WING UAVS |
ICAS2012-11.7.1 |
Quagliotti, F. |
HYBRID GAME EVOLUTIONARY
ALGORITHM FOR MISSION PATH PLANNING OF AERIAL SURVEY TASKS |
ICAS2012-11.7.3 |
Raabe, C. T. |
ADAPTIVE CONTROL INVERSION
AND ACTUATOR FAILURE COMPENSATION FOR UAVS |
ICAS2012-5.2.3 |
Rad, T. |
DYNAMIC SEPARATION MINIMA
COUPLED WITH WAKE VORTEX PREDICTIONS IN DEPENDENT RUNWAY CONFIGURATIONS |
ICAS2012-10.4.2 |
Radchenko, V. N. |
EXPERIMENTAL AND NUMERICAL
INVESTIGATIONS OF LOCAL AERODYNAMICS OF CIVIL AIRCRAFT |
ICAS2012-2.9.4 |
Ragni, D. |
PROPELLER INDUCED GROUND
VORTEX |
ICAS2012-4.10.3 |
Rajef, R. |
AN INVESTIGATION OF MODE I
FRACTURE TOUGHNESS USING ALIGNED CARBON-NANOTUBE FORESTS AT THE CRACK
INTERFACE |
ICAS2012-7.3.2 |
Rajic, N. |
PROBING THE LIMITS - NEW
OPPORTUNITIES IN THERMOELASTIC STRESS ANALYSIS |
ICAS2012-12.1.1 |
Rakotomamonjy, T. |
FAULT DETECTION AND
RECONFIGURATION APPLIED TO A HELICOPTER SWASHPLATE ACTUATOR |
ICAS2012-5.1.2 |
Rambeau, C. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
Rand, O. |
PERFORMANCE ANALYSIS OF A
COAXIAL ROTOR SYSTEM IN HOVER: THREE POINTS OF VIEW |
ICAS2012-2.7.4 |
Rantet, E. |
EOLE, AN INNOVATIVE FLYING
SCALE DEMONSTRATOR FOR AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS |
ICAS2012-1.11.2 |
Rappa, G. |
HYBRID GAME EVOLUTIONARY
ALGORITHM FOR MISSION PATH PLANNING OF AERIAL SURVEY TASKS |
ICAS2012-11.7.3 |
Raps, D. |
EVALUATION AND CORRELATION
OF INTER-LABORATORY RESULTS FROM A RAIN EROSION TEST CAMPAIGN |
ICAS2012-12.2.3 |
Raps, D. |
COMPARATIVE EVALUATION OF
ICING ON AERODYNAMIC SURFACES |
ICAS2012-3.4.3 |
Rasuo, B. |
MANEUVERABILITY OF AN UAV
WITH COANDA EFFECT BASED LIFT PRODUCTION |
ICAS2012-P2.18 |
Ravi, S. |
THE INFLUENCE OF TURBULENCE
INTENSITY ON THE FLOW STRUCTURE OVER A THIN AIRFOIL AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.2 |
Ravi, S. |
OPTIMUM LOCATION OF PRESSURE
MEASUREMENTS AROUND A WING AS A DYNAMIC CONTROL INPUT IN SMOOTH AND TURBULENT
CONDITIONS |
ICAS2012-3.3.3 |
Ray, T. |
ROBUST DESIGN OPTIMIZATION
OF HIGH-PERFORMANCE AXISYMMETRIC SCRAMJETS BASED ON SURROGATE-ASSISTED
EVOLUTIONARY ALGORITHMS |
ICAS2012-4.11.3 |
Razi, M. |
NONLINEAR AEROELASTIC
ANALYSIS OF SWEPT WINGS IN COMPRESSIBLE FLOW VIA THE HARMONIC BALANCE METHOD |
ICAS2012-8.7.1 |
Razin, A. F. |
DEVELOPMENT OF GEODESIC
COMPOSITE AIRCRAFT STRUCTURES |
ICAS2012-8.4.2 |
Reddy, R. |
NUMERICAL AND EXPERIMENTAL
ANALYSIS OF A REPRESENTATIVE ADF HELICOPTER FUSELAGE |
ICAS2012-2.7.2 |
Renaud, G. |
PROBABILISTIC RISK ANALYSIS
FOR AIRCRAFT STRUCTURES WITH LIMITED IN-SERVICE DAMAGES |
ICAS2012-7.9.3 |
Render, P. M. |
A TECHNIQUE TO PREDICT THE
AERODYNAMIC LOSSES OF BATTLE DAMAGED WINGS |
ICAS2012-3.2.2 |
Ress, R. |
FLOW CHARACTERISTICS OF A
HELICOPTER FUSELAGE CONFIGURATION INCLUDING A ROTATING ROTOR HEAD |
ICAS2012-2.7.3 |
Reu, T. K. |
CFD COMPUTATION OF THE
GROUND EFFECT ON AIRPLANE WITH HIGH ASPECT RATIO WING |
ICAS2012-P2.23 |
Reymer, P. |
INTRODUCTION OF A STRUCTURE
INTEGRITY PROGRAM FOR A MILITARY TRAINER AIRCRAFT |
ICAS2012-12.6.2 |
Rezaei, M. |
RISK ASSESSMENT MODELLING
FOR EVALUATING SAFETY AND IMPACT ON BUSINESS VIA A 3D RISK MATRIX |
ICAS2012-P9.2 |
Ricci, S. |
NEOCASS: AN OPEN SOURCE
ENVIRONMENT FOR THE AEROELASTIC ANALYSIS AT CONCEPTUAL DESIGN LEVEL |
ICAS2012-8.10.1 |
Riccobene, L. |
NEOCASS: AN OPEN SOURCE
ENVIRONMENT FOR THE AEROELASTIC ANALYSIS AT CONCEPTUAL DESIGN LEVEL |
ICAS2012-8.10.1 |
Rieger, B. |
FLEXFOIL:
BIO-INSPIRED INTELLIGENT CONTROL ALGORITHM USING ARTIFICIAL NEURAL NETWORKS
FOR WING MORPHING |
ICAS2012-5.4.3 |
Rinoie, K. |
STUDIES ON IMPROVEMENT OF
NONLINEAR PITCHING MOMENT CHARACTERISTICS OF CRANKED-ARROW WING |
ICAS2012-3.2.1 |
Rinoie, K. |
DEVELOPMENT OF LAPTOP PC
TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |
ICAS2012-9.10.ST |
Rizzi, A. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
Roberts, G. |
TETHERING
UNMANNED ROTORCRAFT FOR HIGH-ENDURANCE OPERATIONS |
ICAS2012-P1.3 |
Robertson, M. |
EFFECT ON THE AERODYNAMIC
FORCING IN AN AXIAL TURBINE STAGE ON VARYING STATOR BLADE SHAPE |
ICAS2012-4.3.ST |
Rodde, A. -M. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
Rodzewicz, M. |
DESIGN AND CONFIGURATION
LAYOUTS OF AN ADVANCED LONG ENDURANCE UAV- LESSONS LEARNT AFTER FLIGHT
TESTING |
ICAS2012-1.11.3 |
Roestermundt, D. |
IMPROVING THE PRODUCTION
QUALITY OF THE ADVANCED AUTOMATED FIBER PLACEMENT PROCESS BY MEANS OF ONLINE
PATH CORRECTION |
ICAS2012-6.1.3 |
Rogozin, V. V. |
FLIGHT TESTS OF TRANSPORT
AIRCRAFT UPSET RECOVERY TECHNIQUES AND THE SYSTEM OF INFORMATION SUPPORT OF
CREW |
ICAS2012-5.1.1 |
Rohacs, D. |
RIDE CONTROL FOR THE
PERSONAL PLANE |
ICAS2012-5.3.2 |
Rohacs, J. |
MEASURING AND MODELLING THE
LONGITUDINAL MOTION OF PARAGLIDERS |
ICAS2012-5.10.2 |
Rohacs, J. |
RIDE CONTROL FOR THE
PERSONAL PLANE |
ICAS2012-5.3.2 |
Rohacs, J. |
UNMANNED MEASUREMENT
PLATFORM FOR PARAGLIDERS |
ICAS2012-P1.4 |
Romanelli, G. |
DESIGN AND VERIFICATION OF
FLUTTER SUPPRESSION CONTROL SYSTEMS BY MULTIDISCIPLINARY CO-SIMULATIONS |
ICAS2012-8.7.3 |
Romeo, G. |
PRELIMINARY DESIGN OF A
FUEL-CELL-BASED HYBRID-ELECTRICAL UAV |
ICAS2012-1.8.2 |
Romeo, G. |
VERY-LONG ENDURANCE SOLAR
POWERED AUTONOMOUS UAVS: ROLE AND CONSTRAINTS FOR GMES APPLICATIONS |
ICAS2012-4.7.5 |
Romeo, G. |
MORE/ALL ELECTRIC AIRCRAFT
BASED ON FUEL CELL ENERGY SYSTEM: THE ENFICA-FC EXPERIENCE |
ICAS2012-6.7.2 |
Rona, A. |
STREAMWISE AND CROSSFLOW
INSTABILITIES ON INCLINED CIRCULAR CYLINDERS |
ICAS2012-3.10.2 |
Ronzheimer, A. |
A FULLY AUTOMATED CAD-BASED
FRAMEWORK FOR SHAPE OPTIMIZATION |
ICAS2012-11.10.1 |
Rowlands, D. |
PROBING THE LIMITS - NEW
OPPORTUNITIES IN THERMOELASTIC STRESS ANALYSIS |
ICAS2012-12.1.1 |
Rudenko, S. V. |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
Ruiz-Calavera, L. P. |
CFD BASED AEROELASTIC
CALCULATION OF PROPELLER LOADS |
ICAS2012-9.8.1 |
Ryabov, P. A. |
STUDIES
OF PROPULSION SYSTEM CONCEPTS FOR ADVANCED SUBSONIC AIRLINERS |
ICAS2012-4.7.3 |
Rydell, S.A.H. |
A CASE STUDY OF ARRIVAL AND
DEPARTURE MANAGERS COOPERATION FOR REDUCING AIRBORNE HOLDING TIMES AT
DESTINATION AIRPORTS |
ICAS2012-10.1.ST |
Rye, L. |
ALTERNATIVE AVIATION FUEL
FEEDSTOCK: THE MICROALGAE SOLUTION? |
ICAS2012-8.6.2 |
Ryzhov, A. A. |
ENERGY SUPPLY EFFECT ON
SUPERSONIC BOUNDARY LAYER RECEPTIVITY AND STABILITY |
ICAS2012-P2.21 |
Saad, M. R. |
EXPERIMENTAL STUDIES ON
MICRO-VORTEX GENERATORS IN HYPERSONIC FLOW |
ICAS2012-3.5.2 |
Saad, M. R. |
PERFORMANCE ANALYSIS OF A
SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
ICAS2012-P4.12 |
Saarela, O. |
DIARC PLASMA COATING FOR
RELIABLE AND DURABLE STRUCTURAL BONDING OF METALS |
ICAS2012-7.2.1 |
Sabatini, R. |
A CASE STUDY OF ARRIVAL AND
DEPARTURE MANAGERS COOPERATION FOR REDUCING AIRBORNE HOLDING TIMES AT
DESTINATION AIRPORTS |
ICAS2012-10.1.ST |
Sabatini, R. |
TOWARDS TRAJECTORY
PREDICTION AND OPTIMISATION FOR ENERGY EFFICIENCY OF AN AIRCRAFT WITH
ELECTRICAL AND HYDRAULIC ACTUATION SYSTEMS |
ICAS2012-6.7.3 |
Sabatini, R. |
CORRESPONDENCE AND
CLUSTERING METHODS FOR IMAGE-BASED WING-TIP COLLISION AVOIDANCE TECHNIQUES |
ICAS2012-9.10.4 |
Sabatini, R. |
BI-OBJECTIVE PSEUDOSPECTRAL
OPTIMAL CONTROL TECHNIQUES FOR AIRCRAFT TRAJECTORY OPTIMIZATION |
ICAS2012-P5.6 |
Saddoughi, S. |
THE EFFECT OF PLASMA
ACTUATORS ON TIP CLEARANCE FLOWS IN COMPRESSOR ROTORS |
ICAS2012-4.4.1 |
Saegeler, S. |
IMPROVED MODELLING OF
VORTICAL MIXING FOR THE SIMULATION OF EFFICIENT PROPULSION SYSTEMS |
ICAS2012-4.10.1 |
Sáez, F. J. |
HALA!: TOWARDS HIGHER LEVELS
OF AUTOMATION IN ATM. POSITION PAPER -STATE OF THE ART AND RESEARCH AGENDA |
ICAS2012-10.1.1 |
Saha, A. |
ROBUST DESIGN OPTIMIZATION
OF HIGH-PERFORMANCE AXISYMMETRIC SCRAMJETS BASED ON SURROGATE-ASSISTED
EVOLUTIONARY ALGORITHMS |
ICAS2012-4.11.3 |
Sahai, A. |
AN INTERDISCIPLINARY
APPROACH FOR A VIRTUAL AIR-TRAFFIC SYSTEM SIMULATION FOR SUBJECTIVE
ASSESSMENT IN VR ENVIRONMENTS |
ICAS2012-7.10.3 |
Sahlman, S. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
Sakashita, M. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
Salam, I. R. |
METHODOLOGY FOR A
PRELIMINARY DESIGN STUDY OF A BOX-WING AIRLINER |
ICAS2012-1.10.3 |
Salminen, E. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
Sammut, A. |
RUNWAY CONFLICT ALERTING
DURING TAKE-OFF AND LANDING: ADVISORY OR DIRECTIVE? |
ICAS2012-9.10.1 |
Sampigethaya, K. |
ENHANCING THE "LAST
MILE" COMMUNICATIONS AT AIRPORTS |
ICAS2012-10.10.5 |
Sampigethaya, K. |
BALANCING OPERATOR PRIVACY
AND FUTURE AIRSPACE SURVEILLANCE |
ICAS2012-P8.6 |
Sang, J. H. |
THE
INTEGRATION OPTIMIZATION DESIGN OF AERODYNAMIC AND STEALTH FOR FIGHTERS |
ICAS2012-P2.2 |
Sang, J. H. |
EXPERIMENTAL
INVESTIGATION OF INFRARED STEALTH TECHNOLOGIES OF AERO-ENGINE EXHAUST SYSTEM |
ICAS2012-P4.1 |
Santana, L. D. |
AIRFOIL SELF NOISE REDUCTION
BY APPLICATION OF DIFFERENT TYPES OF TRAILING EDGE SERRATIONS |
ICAS2012-3.11.1 |
Sanz, L. P. |
AIRCRAFT FLIGHT TRAJECTORY
DEVIATION IN THE STANDARD INSTRUMENT DEPARTURES. OPERATORS PENALTIES |
ICAS2012-10.10.2 |
Sarrat, C. |
MODELLING AIR TRAFFIC IMPACT
ON LOCAL AIR QUALITY WITH IESTA AND ADMS-AIRPORT: VALIDATION USING FIELD
MEASUREMENTS ON A REGIONAL AIRPORT |
ICAS2012-4.9.4 |
Sarwe, P. |
MORE ELECTRICAL
ENVIRONMENTAL CONTROL SYSTEM SIMULATION |
ICAS2012-6.6.4 |
Sato, M. |
TRANSITION FLIGHT OF QUAD
TILT WING VTOL UAV |
ICAS2012-11.1.3 |
Sato, T. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
Sato, T. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
Sawa, T. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
Schaefer, M. |
IMPACT OF ALTERNATIVE FUELS
ON ENGINE PERFORMANCE AND CO2-EMISSIONS |
ICAS2012-8.6.3 |
Scharl, J. |
THE GENERALIZED ARRIVAL
PLANNER (GARP): MODELING AND ANALYSIS FOR ARRIVAL PLANNING |
ICAS2012-10.9.3 |
Scharstein, F. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
Schiefele, J. |
OPERATIONAL
HUMAN-IN-THE-LOOP INTEGRATION OF 4D ARRIVAL GUIDANCE |
ICAS2012-5.8.1 |
Schilling, T. |
SYSTEM ANALYSIS OF
PROGNOSTICS AND HEALTH MANAGEMENT SYSTEMS FOR FUTURE TRANSPORT AIRCRAFT |
ICAS2012-12.3.1 |
Schmollgruber, P. |
AIRCRAFT CONCEPTUAL DESIGN
IN A MULTI-LEVEL, MULTI-FIDELITY, MULTI-DISCIPLINARY OPTIMIZATION PROCESS |
ICAS2012-1.6.4 |
Schmollgruber, P. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
Schofield, W. H. |
COLLABORATION CHALLENGES IN
THE GLOBAL AEROSPACE MARKET FOR SMALLER COUNTRIES - AN AUSTRALIAN PERSPECTIVE |
ICAS2012-0.1 |
Scholtz, A. |
OPTIMIZATION OF A NEW
MULTI-PURPOSE UAS FOR SCIENTIFIC APPLICATIONS USING AERODYNAMIC
RECONFIGURATION |
ICAS2012-11.6.4 |
Scholz, D. |
NOVEL LOW-FLYING
PROPELLER-DRIVEN AIRCRAFT CONCEPT FOR REDUCED DIRECT OPERATING COSTS AND
EMISSIONS |
ICAS2012-1.10.5 |
Scholz, O. |
STEADY
AND UNSTEADY FLOWS PAST AIRFOILS AT LOW REYNOLDS NUMBERS IN THE PROXIMITY OF
THE GROUND |
ICAS2012-3.6.ST |
Schönhals, S. |
DYNAMIC SEPARATION MINIMA
COUPLED WITH WAKE VORTEX PREDICTIONS IN DEPENDENT RUNWAY CONFIGURATIONS |
ICAS2012-10.4.2 |
Schrempp, L. |
SHIELDING COSMIC RADIATION
IN AIR TRAFFIC |
ICAS2012-9.6.4 |
Schuhmacher, G. |
MULTIDISCIPLINARY AIRFRAME
DESIGN OPTIMIZATION |
ICAS2012-0.4 |
Schultz, M. |
DYNAMIC TURNAROUND
MANAGEMENT IN A HIGHLY AUTOMATED AIRPORT ENVIRONMENT |
ICAS2012-10.9.2 |
Schumann, U. |
VOLCANIC, WEATHER AND
CLIMATE EFFECTS ON AIR TRANSPORT |
ICAS2012-0.6 |
Schwob, C. |
MODELLING OF IMPACT ON
SANDWICH STRUCTURE FOR FAST MAINTENANCE LOOPS |
ICAS2012-8.3.3 |
Seitz, A. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
Seitz, A. |
PROGRESS AND PERSPECTIVES OF
ELECTRIC AIR TRANSPORT |
ICAS2012-8.6.1 |
Sekimoto, S. |
COMPUTATIONAL STUDY OF A
COMPARISON OF CO-FLOW AND COUNTER BLOWING DBD PLASMA ACTUATOR FOR SEPARATION
CONTROL OVER AN AIRFOIL |
ICAS2012-3.7.4 |
Selivanov, O. D. |
STUDIES
OF PROPULSION SYSTEM CONCEPTS FOR ADVANCED SUBSONIC AIRLINERS |
ICAS2012-4.7.3 |
Send, W. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
Senoguchi, A. |
DEVELOPMENT OF MOBILE
PASSIVE SECONDARY SURVEILLANCE RADAR |
ICAS2012-P8.8 |
Seo, J. |
MULTIPLE UAV FORMATION
RECONFIGURATION WITH COLLISION AVOIDANCE GUIDANCE VIA DIFFERENTIAL GEOMETRY
CONCEPT |
ICAS2012-11.2.2 |
Seong, K. |
HIDDEN MARKOV MODEL
PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
ICAS2012-P6.5 |
Servetnik, A. N. |
ENERGY-BASED METHOD FOR GAS
TURBINE ENGINE DISK BURST SPEED CALCULATION |
ICAS2012-4.1.1 |
Seth, K. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
Seyfang, G. R. |
FANWING -- DEVELOPMENTS AND
APPLICATIONS |
ICAS2012-1.3.3 |
Shadrin, D. V. |
VIBRATION STRENGTH INCREASE
OF ROTATING BLADES USING DYNAMIC SPIN RIGS |
ICAS2012-12.6.4 |
Shakhmatov, E. V. |
THE INSTABILITY OF THE
PIPELINE DUE TO TRANSPORTING FLUID’S PRESSURE RIPPLES |
ICAS2012-8.11.1 |
Shanmugam, J. |
PRODUCTION
OF BIO-FUEL FROM ALGAE BIOMASS, NANNOCHLOROPSIS OCULATA, FOR ADDITION TO
KEROSENE JET A-1 |
ICAS2012-8.6.4 |
Shanygin, A. |
DESIGNING PRO-COMPOSITE
AIRCRAFT CONCEPTS AND LAYOUTS TO MAXIMIZE POTENTIAL BENEFITS OF HIGH SPECIFIC
STRENGTH OF CFRP |
ICAS2012-1.7.3 |
Shanygin, A. N. |
STRENGTH CRITERIA
DEVELOPMENT FOR COMPOSITE STRUCTURES BASING ON SOLUTIONS SUPERPOSITION FOR
MODELS OF DIFFERENT LEVELS |
ICAS2012-7.1.2 |
Sharifzadeh, S. |
DESIGN AND AERO-ELASTIC
OPTIMISATION OF THE STRUCTURE OF THE LAPCAT A2 MACH 5 AIRLINER |
ICAS2012-8.4.3 |
Sharma, M. |
FLEXFOIL:
BIO-INSPIRED INTELLIGENT CONTROL ALGORITHM USING ARTIFICIAL NEURAL NETWORKS
FOR WING MORPHING |
ICAS2012-5.4.3 |
Sharp, P. K. |
INITIAL RESULTS FROM DSTO’S
CORROSION STRUCTURAL INTEGRITY ROADMAP |
ICAS2012-12.6.1 |
Shekhter, A. |
INITIAL RESULTS FROM DSTO’S
CORROSION STRUCTURAL INTEGRITY ROADMAP |
ICAS2012-12.6.1 |
Shelley, A. E. |
PILOT CONVECTIVE WEATHER
DECISION MAKING IN EN ROUTE AIRSPACE |
ICAS2012-10.4.3 |
Shen, Z. |
ON
THE KNEE-POINT PHENOMENON IN COMPOSITE LAMINATES UNDER LOW-VELOCITY IMPACT
AND QUASI-STATIC INDENTATION |
ICAS2012-7.7.ST |
Sheynin, Y. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
Shi, L. |
A GENERAL FOOTPRINT
GENERATION APPROACH FOR LIFTING RE-ENTRY VEHICLE |
ICAS2012-5.7.2 |
Shim, S. -W. |
HIDDEN MARKOV MODEL
PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
ICAS2012-P6.5 |
Shimagaki, M. |
INTEGRATED DESIGN METHOD OF
A ROCKET ENGINE TURBOPUMP SUB-SYSTEM FOR SUPPRESSING ROTOR LATERAL VIBRATION |
ICAS2012-4.3.4 |
Shiomi, K. |
DEVELOPMENT AND EVALUATION
OF FATIGUE AND DROWSINESS PREDICTOR |
ICAS2012-9.6.1 |
Shiomi, K. |
DEVELOPMENT OF MOBILE
PASSIVE SECONDARY SURVEILLANCE RADAR |
ICAS2012-P8.8 |
Shiryaeva, A. A. |
APPLICATION OF THE FAST
CALCULATION TECHNOLOGIES TO SIMULATION OF NON-STATIONARY SUPERSONIC VISCID
FLOW WITH COMBUSTION |
ICAS2012-6.2.3 |
Shmilovich, A. |
HIGH-LIFT SYSTEMS FOR
ENHANCED TAKEOFF PERFORMANCE |
ICAS2012-9.5.1 |
Shoji, H. |
EVALUATION ON DISCRETE
SOURCE DAMAGES OF CFRP STIFFENED PANELS |
ICAS2012-7.7.1 |
Shurman, V. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
Shvirev, A. A. |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
Si, J. |
THE STUDY ON THE AIRCRAFT
INTEGRATED CHARACTERS WITH DIFFERENT HEIGHT WINGLETS |
ICAS2012-P2.9 |
Si, J. T. |
THE COMPREHENSIVE STUDY ON
ADVANCED WINGTIP DEVICES IN LARGE CIVIL AIRCRAFT |
ICAS2012-8.8.3 |
Sibilski, K. |
A HIGHLY EXPANDABLE LOW-COST
OPEN-SOURCE UAV SYSTEM WITH HIGH ON-BOARD PROCESSING POWER |
ICAS2012-1.8.1 |
Sichev, V. K. |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
Siddens, A. J. |
DETAILED POST-SOFT IMPACT
PROGRESSIVE DAMAGE ANALYSIS FOR A HYBRID STRUCTURE JET ENGINE |
ICAS2012-4.2.3 |
Siddens, A. J. |
COUPLED
MICROMECHANICS-FINITE ELEMENT PROGRESSIVE FAILURE DYNAMIC ANALYSIS APPROACH:
F-16 CANOPY CASE STUDY |
ICAS2012-7.7.5 |
Sidoryuk, M. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
Siikonen, T. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
Silva, S. S. |
CATEGORIZATION OF UNRELIABLE
AIRSPEED EVENTS USING RASMUSSEN’S HUMAN PERFORMANCE MODEL |
ICAS2012-9.4.4 |
Simkins, D. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
Simon, P. |
IMPROVEMENTS FOR OPTIMUM
PROFILE SCHEDULING OF USER PREFERRED TRAJECTORIES |
ICAS2012-10.3.2 |
Sizmann, A. |
PROGRESS AND PERSPECTIVES OF
ELECTRIC AIR TRANSPORT |
ICAS2012-8.6.1 |
Sizmann, A. |
SHIELDING COSMIC RADIATION
IN AIR TRAFFIC |
ICAS2012-9.6.4 |
Skomorokhov, S. I. |
AN EXPERIENCE IN AERODYNAMIC
DESIGN OF TRANSPORT AIRCRAFT |
ICAS2012-2.9.3 |
Slobodkina, F. A. |
NUMERICAL MODELING OF FLOW
IN GASDYNAMIC RESONATOR AND MODEL VALIDATION BY RESULTS OF PULSE ENGINE TESTS |
ICAS2012-P4.10 |
Smaili, H. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
Smart, M. |
HIFIRE: AN INTERNATIONAL COLLABORATION TO ADVANCE THE SCIENCE AND TECHNOLOGY OF HYPERSONIC FLIGHT |
ICAS2012-0.8 |
Smart, M. K. |
STREAMWISE PORTHOLE FUEL
INJECTION FOR BOUNDARY-LAYER COMBUSTION INSIDE A SCRAMJET ENGINE |
ICAS 2012-P4.16 |
Smith, D. D. |
COMPUTATIONAL AND
EXPERIMENTAL ANALYSIS OF THE ACTIVE MORPHING WING CONCEPT |
ICAS2012-2.5.3 |
Smrcek, L. |
ADVANCE SEAPLANE CONCEPTUAL
DESIGN ADAPTING TRIMARAN BOAT HULL CONCEPT |
ICAS2012-2.1.3 |
Söderberg, R. |
ROBUST LIFECYCLE
OPTIMIZATION OF TURBINE COMPONENTS USING SIMULATION PLATFORMS |
ICAS2012-4.3.2 |
Soemarwoto, B. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
Sohier, H. |
EOLE, AN INNOVATIVE FLYING
SCALE DEMONSTRATOR FOR AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS |
ICAS2012-1.11.2 |
Solcia, T. |
DESIGN AND VERIFICATION OF
FLUTTER SUPPRESSION CONTROL SYSTEMS BY MULTIDISCIPLINARY CO-SIMULATIONS |
ICAS2012-8.7.3 |
Soltani, Z. |
WAVELET-BASED ACTIVE SENSING
FOR QUANTITATIVE ASSESSMENT OF THROUGH-THICKNESS CRACK SIZE AND ANGLE IN
COMPOSITE PLATES |
ICAS2012-P3.8 |
Song, B. |
AERODYNAMICS ANALYSIS OF
CYCLOIDAL ROTOR |
ICAS2012-2.7.1 |
Song, B. F. |
NUMERICAL STUDY OF PITCHING
OSCILLATION EFFECT ON AERODYNAMIC CHARACTERISTICS OVER ASYMMETRIC VORTEX
STRUCTURE OF SLENDER REVOLUTION |
ICAS2012-2.5.2 |
Song, J. |
FLOW CONTROL USING DBD
PLASMA ON BACKWARD-FACING STEP |
ICAS2012-3.7.3 |
Song, J. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
Song, W. -J. |
A NEW METHOD OF CALCULATION
THE DELAY TIME OF MULTI-CREW MEMBER EJECTION |
ICAS2012-P6.2 |
Song, W. P. |
COMPARISON OF INFILL
SAMPLING CRITERIA IN KRIGING-BASED AERODYNAMIC OPTIMIZATION |
ICAS2012-11.10.ST |
Song, W. P. |
LAMINAR FLOW WING’S
OPTIMIZATION DESIGN BY RANS SOLVER WITH AUTOMATIC TRANSITION PREDICTION |
ICAS2012-2.2.3 |
Song, W. -P. |
DESIGN OF LAMINAR
SUPERCRITICAL AIRFOILS BASED ON NAVIER-STOKES EQUATIONS |
ICAS2012-2.2.2 |
Sosebee, P. D. |
WATER TUNNEL FORCE AND
MOMENT STUDIES OF A MANEUVERING UCAV 1303 AND THEIR CONTROL |
ICAS2012-3.1.3 |
Soudakov, V. G. |
EXPERIMENTAL AND NUMERICAL
INVESTIGATIONS OF LOCAL AERODYNAMICS OF CIVIL AIRCRAFT |
ICAS2012-2.9.4 |
Soudakov, V. G. |
ENERGY SUPPLY EFFECT ON
SUPERSONIC BOUNDARY LAYER RECEPTIVITY AND STABILITY |
ICAS2012-P2.21 |
Soulat, L. |
MULTI-OBJECTIVE OPTIMIZATION
OF MULTI-ELEMENT HIGH-LIFT AIRFOIL |
ICAS2012-2.3.4 |
Soulat, L. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
Sridhar, B. |
UNCERTAINTY QUANTIFICATION
IN THE DEVELOPMENT OF AVIATION OPERATIONS TO REDUCE AVIATION EMISSIONS AND
CONTRAILS |
ICAS2012-7.10.2 |
Staack, I. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
Staack, I. |
MORE ELECTRICAL
ENVIRONMENTAL CONTROL SYSTEM SIMULATION |
ICAS2012-6.6.4 |
Stalewski, W. |
OPTIMISATION OF THE
HELICOPTER FUSELAGE WITH SIMULATION OF MAIN AND TAIL ROTOR INFLUENCE |
ICAS2012-1.4.1 |
Stanfield, S. |
HIFIRE-1 BOUNDARY-LAYER
TRANSITION MEASUREMENTS |
ICAS2012-3.10.3 |
Stanisak, M. |
GBAS CURVED APPROACH
PROCEDURES: ADVANTAGES, CHALLENGES AND APPLICABILITY |
ICAS2012-4.9.2 |
Stanley, D. S. |
NON-LINEAR BEHAVIOUR OF A
WING DUE TO UNDERWING STORES |
ICAS2012-10.6.ST2 |
Steen, M. |
GBAS CURVED APPROACH
PROCEDURES: ADVANTAGES, CHALLENGES AND APPLICABILITY |
ICAS2012-4.9.2 |
Stefaniak, D. |
SEMI-ANALYTICAL SPRING-IN
ANALYSIS TO COUNTERACT CFRP MANUFACTURING DEFORMATIONS BY TOOL COMPENSATION |
ICAS2012-8.2.2 |
Steiner, H.-J. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
Stephani, P. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
Stepniczka, I. |
HMIAC – SURVEY ON
HUMAN-MACHINE INTERACTION IN AIRCRAFT COCKPITS |
ICAS2012-9.7.4 |
Stokes, N. |
EXTERNAL AERODYNAMIC
PRESSURE LOADS FOR A RIGID FIGHTER AIRCRAFT, A COMPARISON BETWEEN PSP AND CFD |
ICAS2012-10.6.2 |
Stokes, N. |
BOUNDARY LAYER TRANSITION
DETECTION USING TEMPERATURE SENSITIVE PAINT IN THE ARA TRANSONIC WIND TUNNEL |
ICAS2012-3.4.2 |
Storm, T. M. |
BEYOND TWO-EQUATION
TURBULENCE MODELING FOR THE REYNOLDS-AVERAGED NAVIER-STOKES EQUATIONS:
ADVANCES IN COMPLEX FLOW PREDICTIONS |
ICAS2012-2.4.1 |
Strobl, T. |
COMPARATIVE EVALUATION OF
ICING ON AERODYNAMIC SURFACES |
ICAS2012-3.4.3 |
Stroehlein, T. |
DESIGN, DEVELOPMENT AND
MANUFACTURING OF THE ALCAS CFRP DOOR SURROUND STRUCTURE |
ICAS2012-8.8.1 |
Stückl, S. |
VOLTAIR - THE ALL ELECTRIC
PROPULSION CONCEPT PLATFORM – A VISION FOR ATMOSPHERIC FRIENDLY FLIGHT |
ICAS2012-4.7.2 |
Stumpf, E. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
Stumpf, E. |
AN INTERDISCIPLINARY
APPROACH FOR A VIRTUAL AIR-TRAFFIC SYSTEM SIMULATION FOR SUBJECTIVE
ASSESSMENT IN VR ENVIRONMENTS |
ICAS2012-7.10.3 |
Su, B. |
CRACK NUCLEATION MODELING IN
NOTCHED SPECIMEN SUBJECTED TO HIGH FATIGUE LOADING |
ICAS2012-7.7.4 |
Subbaramaiah, R. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
Sugimoto, S. |
EVALUATION ON DISCRETE
SOURCE DAMAGES OF CFRP STIFFENED PANELS |
ICAS2012-7.7.1 |
Sun, F. -L. |
THE FABRICATION AND
CHARACTERIZATION OF TiO2 UV DETECTOR |
ICAS2012-7.3.ST |
Sun, J. N. |
STUDY OF THE PRESSURE DROP
FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
ICAS2012-4.4.ST |
Sun, J. Y. |
INVESTIGATION OF AIRBORNE
PRODUCT EXPENDING DYNAMIC CALIBRATION LIFE METHODS |
ICAS2012-12.5.2 |
Sun, S. |
MICROSTRUCTURE AND
MECHANICAL PROPERTIES OF LASER CLADDING REPAIR OF AISI 4340 STEEL |
ICAS2012-12.4.4 |
Sun, X. |
TECHNOLOGY ASSESSMENT OF
FUTURE AIRCRAFT: SOCIO-ECO-EFFICIENCY IN CONCEPTUAL AIRCRAFT DESIGN |
ICAS2012-1.9.2 |
Sun, X. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
Sun, Y. -F. |
A PRELIMINARY CFD
INVESTIGATION ON REAR FUSELAGE SUPPORT CORRECTION |
ICAS2012-P2.14 |
Sundaresan, C. |
A METHODOLOGY FOR PARAMETRIC
PRODUCTION PLANNING IN PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-6.4.4 |
Surini, A. |
EXPERIMENTAL AND NUMERICAL
ASSESSMENT OF HELICOPTER SUBFLOOR CRASHWORTHINESS |
ICAS2012-8.1.1 |
Suvorova, E. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
Suzuki, A. |
DEVELOPMENT AND EVALUATION
OF FATIGUE AND DROWSINESS PREDICTOR |
ICAS2012-9.6.1 |
Suzuki, H. |
GUIDANCE AND CONTROL LAW FOR
D-SEND#2 |
ICAS2012-5.3.1 |
Suzuki, S. |
HIGH ANGLE OF ATTACK FLIGHT
CONTROL OF A TAIL-SITTER UNMANNED AIRCRAFT |
ICAS2012-11.8.2 |
Suzuki, S. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
Suzuki, S. |
INSIDE THE PILOTS MIND:
VISUAL INFORMATION USE IN MANUAL AIRCRAFT LANDINGS |
ICAS2012-9.7.1 |
Suzuki, S. |
SCIENCE AND TECHNOLOGY MAP
ANALYSIS OF AEROSPACE ENGINEERING |
ICAS2012-P7.1 |
Svirsky, Y. |
OUTLINE OF AIRCRAFT
STRUCTURE HEALTH AND USAGE MONITORING SYSTEMS AND METHODS USED FOR THEIR
REALIZATIONS |
ICAS2012-12.1.2 |
Swieringa, K. |
INTERVAL MANAGEMENT WITH
SPACING TO PARALLEL DEPENDENT RUNWAYS (IMSPIDR) EXPERIMENT AND RESULTS |
ICAS2012-9.10.3 |
Szolloz, A. |
GLOBAL OPTIMIZATION OF
TWO-DIMENSIONAL HIGH LIFT AERODYNAMIC SYSTEM |
ICAS2012-11.10.2 |
Tahk, M. -J. |
CONTROLLER DESIGN AND
ANALYSIS OF UNMANNED AERIAL VEHICLES USING AUTOMATIC GAIN GENERATION
TECHNIQUE |
ICAS2012-11.8.1 |
Tahk, M. -J. |
A PEG-BASED ASCENDING
GUIDANCE ALGORITHM FOR RAMJET-POWERED VEHICLES |
ICAS2012-5.7.4 |
Tahk, M. -J. |
AUTOPILOT DESIGN FOR AN
AGILE MISSILE USING L1 ADAPTIVE BACKSTEPPING CONTROL |
ICAS2012-P5.4 |
Tahk, M. -J. |
UAV COLLISION AVOIDANCE VIA
OPTIMAL TRAJECTORY GENERATION METHOD |
ICAS2012-P5.5 |
Tahk, M. -J. |
TERRAIN REFERENCED UAV
NAVIGATION WITH LIDAR - A COMPARISON OF SEQUENTIAL PROCESSING AND BATCH
PROCESSING ALGORITHMS |
ICAS2012-P5.7 |
Tahk, M. -J. |
HIDDEN MARKOV MODEL
PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
ICAS2012-P6.5 |
Takahashi, N. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
Takahashi, R. |
FORMATION SHAPE CONTROL OF
UNMANNED AIR VEHICLES |
ICAS2012-P5.8 |
Takalani, L. S. |
A PRACTICAL, ROUTE-BASED
APPROACH TO AIRSPACE CAPACITY MANAGEMENT |
ICAS2012-10.2.2 |
Takanobu, H. |
GUST RESPONSE ANALYSIS IN
THE FLIGHT FORMATION OF UNMANNED AIR VEHICLES |
ICAS2012-P5.9 |
Takeda, S. |
EVALUATION ON DISCRETE
SOURCE DAMAGES OF CFRP STIFFENED PANELS |
ICAS2012-7.7.1 |
Takeichi, N. |
FUNDAMENTAL CHARACTERISTICS
OF DECENTRALIZED AIR TRAFFIC FLOW CONTROL IN HIGH DENSITY CORRIDOR |
ICAS2012-10.7.2 |
Takeichi, N. |
CONTINUOUS DESCENT
TRAJECTORY WITH OPTIMUM ARRIVAL TIME CONTROLLABILITY |
ICAS2012-P8.3 |
Takovitskii, S. A. |
ELLIPTICALLY CONICAL TWIST
AND CAMBER OF DELTA WINGS |
ICAS2012-2.8.2 |
Talbotec, J. |
STUDY ON NOISE OF COUNTER
ROTATING FAN MODELS AT CIAM ANECHOIC CHAMBER |
ICAS2012-3.9.4 |
Tamagnone Cosmelli, F. |
MULTIDISCIPLINARY DESIGN AND
FLIGHT TESTING OF A REMOTE GAS/PARTICLE AIRBORNE SENSOR SYSTEM |
ICAS2012-6.10.4 |
Tan, Z. |
RESEARCH FOR JET FLOW INFLUENCES TO WING-MOUNTED CIVIL
AIRCRAFT AERODYNAMIC CHARACTERISTICS |
ICAS2012-2.9.1 |
Tanaka, N. |
VISUALIZATION OF UNSTEADY
BEHAVIOR OF SHOCK WAVES AROUND SUPERSONIC INTAKE INSTALLED IN SHOCK TUNNEL |
ICAS2012-P4.5 |
Tanatsugu, N. |
DEVELOPMENT OF A SMALL-SCALE
SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED |
ICAS2012-1.2.2 |
Tang, J. |
AERODYNAMICS ANALYSIS OF
CYCLOIDAL ROTOR |
ICAS2012-2.7.1 |
Tang, M. |
CHARACTERISTICS
OF AN 80-DEG SWEPT DELTA WING IN WING ROCK OR FREE YAWING |
ICAS2012-3.1.ST1 |
Tang, M. Z. |
FLOW
CONTROL TEST RESEARCH OF AIRCRAFT MODEL WITH ADJUSTABLE CANAEDS |
ICAS2012-P2.5 |
Tang, Z. |
A METHODOLOGY FOR PARAMETRIC
PRODUCTION PLANNING IN PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-6.4.4 |
Tani, Y. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
Tao, C. H. |
FRACTURE
ANALYSIS OF BLADE DOVETAIL OF TC11 TITANIUM ALLOY |
ICAS2012-P4.7 |
Tarasov, A. I. |
NUMERICAL MODELING OF FLOW
IN GASDYNAMIC RESONATOR AND MODEL VALIDATION BY RESULTS OF PULSE ENGINE TESTS |
ICAS2012-P4.10 |
Taylor, S. |
BALANCING OPERATOR PRIVACY
AND FUTURE AIRSPACE SURVEILLANCE |
ICAS2012-P8.6 |
Techakesari, O. |
DESIGN OF FLIGHT AVOIDANCE
MANOEUVRE ALPHABETS FOR MIXED CENTRALISED-DECENTRALISED SEPARATION MANAGEMENT |
ICAS2012-10.7.3 |
Teimouri, B. |
RISK ASSESSMENT MODELLING
FOR EVALUATING SAFETY AND IMPACT ON BUSINESS VIA A 3D RISK MATRIX |
ICAS2012-P9.2 |
Tenno, T. |
DESIGN OF ROBUST FLIGHT
CONTROL SYSTEM FOR SMALL FIXED-WING UAV |
ICAS2012-11.9.3 |
Tervakangas, S. |
DIARC PLASMA COATING FOR
RELIABLE AND DURABLE STRUCTURAL BONDING OF METALS |
ICAS2012-7.2.1 |
Tetzloff, I. J. |
MEASURING SYSTEM-WIDE
IMPACTS OF NEW AIRCRAFT ON THE ENVIRONMENT |
ICAS2012-7.11.1 |
Tezuka, A. |
DEVELOPMENT OF LAPTOP PC
TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |
ICAS2012-9.10.ST |
Thielecke, F. |
MODEL BASED DESIGN AND
EXPERIMENTAL VALIDATION OF ELECTRO-MECHANIC ACTUATOR SYSTEMS FOR A NOSE
LANDING GEAR |
ICAS2012-6.8.3 |
Thomas, P. J. |
ON THE EFFECT OF DISTRIBUTED
ROUGHNESS ON TRANSITION OVER ROTOR-STATOR DEVICES |
ICAS2012-3.10.4 |
Thomson, D. G. |
ASSESSING
HELICOPTER SURVIVABILITY TO GROUND LAUNCHED PROJECTILES USING MULTI-FIDELITY
INVERSE SIMULATION |
ICAS2012-1.4.4 |
Thomson, R. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
Thomson, R. |
DIRECTIONAL ENHANCEMENT OF
COMPOSITE STRUCTURES ENERGY ABSORPTION USING MAGNETORHEOLOGICAL FLUIDS |
ICAS2012-7.8.1 |
Thomson, R. |
IMPROVED DESIGN METHODS FOR
CRASHWORTHY COMPOSITE HELICOPTER STRUCTURES |
ICAS2012-8.1.2 |
Thomson, R. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
Thouault, N. |
AEROACOUSTIC ANALYSIS OF A
HELICOPTER CONFIGURATION WITH DUCTED TAIL ROTOR |
ICAS2012-3.9.1 |
Timokhin, V. |
AEROELASTIC
MULTIDISCIPLINARY ANALYSIS OF THE FIN
WITH INNOVATIVE ADAPTIVE CONTROL |
ICAS2012-8.7.4 |
Tisato, J. |
APPLICATION OF THE RANGE
SAFETY TEMPLATE TOOLKIT TO UAS RISK HAZARD ANALYSES SUPPORTING AIRWORTHINESS
REGULATION |
ICAS2012-9.2.3 |
Tobin, E. F. |
EVALUATION AND CORRELATION
OF INTER-LABORATORY RESULTS FROM A RAIN EROSION TEST CAMPAIGN |
ICAS2012-12.2.3 |
Tobin, E. F. |
LABORATORY TESTING OF INSECT
CONTAMINATION FOR LAMINAR FLOW APPLICATIONS USING AN INSECT-IMPACT TEST
FACILITY |
ICAS2012-3.4.4 |
Toebben, H. H. |
FLIGHT TESTING OF NOISE
ABATING RNP PROCEDURES AND STEEP APPROACHES |
ICAS2012-4.9.1 |
Tokutake, H. |
THE FLAPPING AIRCRAFT
DYNAMICS WITH WING DEFORMATION UNDER GUST INPUT |
ICAS2012-11.9.2 |
Tomczyk, A. |
CONTROL AUGMENTATION SYSTEM
FOR REMOTE STEERING UAV |
ICAS2012-6.9.3 |
Tomczyk, A. |
MODEL FOLLOWING TOTAL IN
FLIGHT SIMULATOR AS AN EDUCATIONAL TOOL |
ICAS2012-P5.1 |
Tong, L. |
DESIGN CONSIDERATIONS OF A
PRESSURE DRIVEN MORPHING WING STRUCTURE |
ICAS2012-8.4.1 |
Toor, J. van |
VOLTAIR - THE ALL ELECTRIC
PROPULSION CONCEPT PLATFORM – A VISION FOR ATMOSPHERIC FRIENDLY FLIGHT |
ICAS2012-4.7.2 |
Torabi, A. |
EFFECT OF LATERAL PLACEMENT
OF CERAMIC AND METAL GRAINS ON THERMAL STRESS DISTRIBUTION THROUGHOUT FGMS |
ICAS2012-7.3.4 |
Toratani, D. |
RESEARCH AND DEVELOPMENT OF
DOUBLE TETRAHEDRON HEXA-ROTORCRAFT (DOT-HR) |
ICAS2012-1.4.2 |
Toratani, D. |
COLLISION AVOIDANCE OF
INDOOR FLYING DOUBLE TETRAHEDRON HEXA-ROTORCRAFT |
ICAS2012-11.5.1 |
Torii, H. |
THE EXTENSION OF
DISCRETE-TIME FLUTTER MARGIN |
ICAS2012-8.5.2 |
Törner, S. |
IMPLEMENTING TIME BASED CDA
OPERATIONS IN A MEDIUM-HIGH DENSITY ATM ENVIRONMENT |
ICAS2012-10.8.1 |
Toussaint, C. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
Tran, T. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
Travaglini, L. |
NEOCASS: AN OPEN SOURCE
ENVIRONMENT FOR THE AEROELASTIC ANALYSIS AT CONCEPTUAL DESIGN LEVEL |
ICAS2012-8.10.1 |
Tripero, A. M. G. |
WEIGHT ON WHEEL SYSTEM BASED
ON STRAIN GAUGES |
ICAS2012-6.11.2 |
Tristrant, D. |
FAULT DETECTION AND
RECONFIGURATION APPLIED TO A HELICOPTER SWASHPLATE ACTUATOR |
ICAS2012-5.1.2 |
Troncone, E. |
IDENTIFICATION OF HELICOPTER
GROUND RESONANCE WITH MULTI-BODY SIMULATION |
ICAS2012-8.3.2 |
Truss, R. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
Tshuchiya, T. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
Tsourdos, A. |
MULTIPLE UAV FORMATION
RECONFIGURATION WITH COLLISION AVOIDANCE GUIDANCE VIA DIFFERENTIAL GEOMETRY
CONCEPT |
ICAS2012-11.2.2 |
Tumanov, N. V. |
PREVENTION OF LOW CYCLE
FATIGUE FRACTURE OF AVIATION ENGINE CRITICAL PARTS |
ICAS2012-4.1.2 |
Tupper, A. |
MANAGING DIFFUSE ERUPTION
CLOUDS - THE EXPERIENCES OF 2010-11, AND THE RESULTS OF THE INTERNATIONAL
VOLCANIC ASH TASK FORCE |
ICAS2012-0.7 |
Tuss, J. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
Tutty, M. G. |
A RECENT HISTORY OF THE
EVOLUTION OF AUSTRALIA’S AERODYNAMICS STORE SEPARATION CAPABILITY – THROUGH
INDIGENOUS AND INTERNATIONAL PROGRAMS |
ICAS2012-10.6.4 |
Ubadike, O. C. |
FUZZY LOGIC BASED FLIGHT
CONTROL SYSTEM FOR THE NIGERIAN AIR FORCE AIR BEETLE AIRCRAFT |
ICAS2012-P5.12 |
Ucan, H. |
SENSOR AND
REAL-TIME-PROCESS-SIMULATION GUIDED AUTOCLAVE PROCESS CONTROL FOR COMPOSITE
PRODUCTION |
ICAS2012-6.1.2 |
Uchiumi, M. |
INTEGRATED DESIGN METHOD OF
A ROCKET ENGINE TURBOPUMP SUB-SYSTEM FOR SUPPRESSING ROTOR LATERAL VIBRATION |
ICAS2012-4.3.4 |
Uchiyama, K. |
DESIGN OF ROBUST FLIGHT
CONTROL SYSTEM FOR SMALL FIXED-WING UAV |
ICAS2012-11.9.3 |
Udzhukhu, A. Y. |
ADVANCED AEROSPACE SYSTEMS
WITH INTERCONTINENTAL AND GLOBAL RANGE OF FLIGHT |
ICAS2012-1.5.2 |
Ueda, Y. |
STABILITY ANALYSIS ON
NATURAL LAMINAR FLOW WING IN SUPERSONIC FLOW: ONERA-JAXA JOINT RESEARCH
PROGRAM |
ICAS2012-3.10.1 |
Uejima, K. |
ANALYZING SEPARATION LOSS
EVENTS IN TWO-PAIRED AIRCRAFT TRAILING CONDUCTING AIRBORNE TIME SPACING BASED
CONTINUOUS DESCENT ARRIVAL |
ICAS2012-10.8.3 |
Ueno, A. |
SIMULTANEOUS OPTIMIZATION OF
AIRFRAME AND ENGINE FOR SUPERSONIC TRANSPORT |
ICAS2012-12.3.4 |
Ueno, M. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
Ueno, S. |
COLLISION AVOIDANCE OF
INDOOR FLYING DOUBLE TETRAHEDRON HEXA-ROTORCRAFT |
ICAS2012-11.5.1 |
Uher, O. |
THE CFRP SAILPLANE WING
SEGMENTS MANUFACTURED BY FILAMENT PLACEMENT |
ICAS2012-7.5.ST |
Unay, E. |
METHODS FOR EVALUATION OF
AIRCRAFT MASS DISTRIBUTION |
ICAS2012-1.1.3 |
Unay, E. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
Urik, T. |
THE CFRP SAILPLANE WING
SEGMENTS MANUFACTURED BY FILAMENT PLACEMENT |
ICAS2012-7.5.ST |
Uspensky, A. A. |
INFLUENCE OF TURBULENCE
SCALE AND SHAPE OF LEADING EDGE ON FST-INDUCED LAMINAR-TURBULENT TRANSITION |
ICAS2012-2.4.3 |
Ustinov, M. V. |
INFLUENCE OF TURBULENCE
SCALE AND SHAPE OF LEADING EDGE ON FST-INDUCED LAMINAR-TURBULENT TRANSITION |
ICAS2012-2.4.3 |
Uzunoglu, A. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
Vadillo, J. L. |
ACTIVE
CONTROL OF SHOCK/BOUNDARY LAYER INTERACTION FOR TRANSONIC DRAG REDUCTION OF
AIRFOILS |
ICAS2012-2.10.4 |
Valiyff, A. |
FLEXIBILITY OF AN ORITHOPTER
WING TESTED IN A WIND-TUNNEL |
ICAS2012-12.5.3 |
van den Berg, T. |
AUTOMATIC FLATTENING OF THREE-DIMENSIONAL WIRING HARNESSES FOR
MANUFACTURING |
ICAS2012-6.4.2 |
Van den Brink, W. |
BUCKLING-OPTIMIZED VARIABLE
STIFFNESS LAMINATES FOR A COMPOSITE FUSELAGE WINDOW SECTION |
ICAS2012-8.9.3 |
van der Hoogt, P. |
ACCELERATED LIFE CONSUMPTION
DUE TO THERMO-ACOUSTIC OSCILLATIONS IN GAS TURBINES: XFEM & CRACK |
ICAS2012-4.2.2 |
van der Windt, M. |
CURFEWS AT INTERNATIONAL
AIRPORTS - A STUDY OF CURRENT PRACTICE |
ICAS2012-10.5.3 |
van Dommelen, J. |
A CONCEPTUAL DESIGN AND
ANALYSIS TOOL FOR BLENDED WING BODY AIRCRAFT |
ICAS2012-1.7.2 |
van Tooren, M. J. L. |
AUTOMATIC FLATTENING OF THREE-DIMENSIONAL WIRING HARNESSES FOR
MANUFACTURING |
ICAS2012-6.4.2 |
Vandewater, L. A. |
BI-AXIAL VIBRATION ENERGY
HARVESTING FOR USE ON AEROSPACE PLATFORMS |
ICAS2012-6.7.1 |
Vandi, L. -J. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
Vankan, W. J. |
BUCKLING-OPTIMIZED VARIABLE
STIFFNESS LAMINATES FOR A COMPOSITE FUSELAGE WINDOW SECTION |
ICAS2012-8.9.3 |
Vanneste, T. |
AEROELASTIC SIMULATION OF
FLEXIBLE FLAPPING WING BASED ON STRUCTURAL FEM AND QUASI-STEADY AERODYNAMIC
MODEL |
ICAS2012-8.5.1 |
Vanuchi, P. |
WIND TUNNEL TESTING OF
POROUS DEVICES FOR THE REDUCTION OF FLAP SIDE-EDGE NOISE |
ICAS2012-9.11.2 |
Varley, R. V. |
DELAMINATION TOUGHENING OF
CARBON-EPOXY LAMINATE WITH A POLYETHYLENE-CO-METHACRYLIC ACID (EMAA)
SELF-HEALING MODIFIER |
ICAS2012-7.6.2 |
Vasiliev, V. V. |
DEVELOPMENT OF GEODESIC
COMPOSITE AIRCRAFT STRUCTURES |
ICAS2012-8.4.2 |
Vasilyev, B. |
PREDICTION OF THE KINETICS
OF THE 3D STRESS-STRAIN STATE OF HIGH-TEMPERATURE GAS TURBINE BLADES WITH
LIMITED EXPERIMENTAL DATA |
ICAS2012-4.2.1 |
Vasista, S. |
DESIGN CONSIDERATIONS OF A
PRESSURE DRIVEN MORPHING WING STRUCTURE |
ICAS2012-8.4.1 |
Vaughn, L. |
COMPOSITE SANDWICH PANEL
BIRDSTRIKE TESTING AND ANALYSIS |
ICAS2012-8.3.4 |
Vedeshkin, G. K. |
EXPERIMENTAL INVESTIGATIONS
OF HYDRAULIC DEVICES PERFORMANCE IN AVIATION ENGINE COMPARTMENT |
ICAS2012-P2.10 |
Veidt, M. |
FINITE ELEMENT SIMULATION OF
CRACK PROPAGATION IN MILITARY AIRCRAFT COATINGS |
ICAS2012-7.2.3 |
Veidt, M. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
Veldhuis, L. |
PROPELLER INDUCED GROUND
VORTEX |
ICAS2012-4.10.3 |
Veldhuis, L. L. M. |
NOVEL PASSIVE AND ACTIVE
FLOW CONTROL FOR HIGH LIFT |
ICAS2012-3.7.2 |
Venediktov, V. D. |
INTERDISCIPLINARY COMPLEX
DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES |
ICAS2012-4.3.3 |
Venediktov, V. D. |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
Venkatraman, K. |
TRANSONIC FLUTTER, SHOCKS,
AND PARAMETER EFFECTS |
ICAS2012-2.6.4 |
Verseux, O. |
EXPERIMENTAL INVESTIGATIONS
OF HYDRAULIC DEVICES PERFORMANCE IN AVIATION ENGINE COMPARTMENT |
ICAS2012-P2.10 |
Verstraete, D. |
PRELIMINARY DESIGN OF A
FUEL-CELL-BASED HYBRID-ELECTRICAL UAV |
ICAS2012-1.8.2 |
Verstraete, D. |
DESIGN AND TEST OF A UAV
BLENDED WING BODY CONFIGURATION |
ICAS2012-1.8.3 |
Verstraete, D. |
HARDWARE-IN-THE-LOOP
SIMULATION OF FUEL-CELL-BASED HYBRID-ELECTRICAL UAV PROPULSION |
ICAS2012-4.5.2 |
Verstraete, D. |
DESIGN AND AERO-ELASTIC
OPTIMISATION OF THE STRUCTURE OF THE LAPCAT A2 MACH 5 AIRLINER |
ICAS2012-8.4.3 |
Verstraete, D. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
Vich, O. |
EIGENVALUE AND FLUTTER
SENSITIVITY ANALYSIS OF AIRLINER WING |
ICAS2012-P3.1 |
Ville, F. |
COUPLING MECH. & THERMAL
MODELS IN PRELIMINARY DESIGN OF POWER TRANSMISSIONS DRIVEN BY THERMAL ISSUES |
ICAS2012-6.6.1 |
Vine, J. |
LOAD SYNTHESIS OF HELICOPTER
DYNAMIC COMPONENTS: IMPROVEMENTS TO LINEAR REGRESSION IN THE AZIMUTH DOMAIN |
ICAS2012-8.10.ST |
Vio, G. A. |
NON-LINEAR BEHAVIOUR OF A
WING DUE TO UNDERWING STORES |
ICAS2012-10.6.ST2 |
Vio, G. A. |
DESIGN OF COMPOSITE
STRUCTURES FOR IMPROVED AEROELASTIC PERFORMANCE |
ICAS2012-8.4.4 |
Vio, G. A. |
AEROELASTIC RESPONSE OF A
CHORDWISE FLEXIBLE WINGS SUBJECTED TO GUSTS: AN INITIAL STUDY ON EXPERIMENTAL
AND COMPUTATIONAL VALIDATION |
ICAS2012-8.5.3 |
Viviani, A. |
DESIGN OF MASS SAVING
CONFIGURATIONS FOR WINGED REENTRY VEHICLES |
ICAS2012-1.5.3 |
Viviani, A. |
AEROTHERMODYNAMIC FIELD PAST
A REENTRY CAPSULE FOR SAMPLE RETURN MISSIONS |
ICAS2012-3.8.1 |
Vlasenko, V. V. |
APPLICATION OF THE FAST
CALCULATION TECHNOLOGIES TO SIMULATION OF NON-STATIONARY SUPERSONIC VISCID
FLOW WITH COMBUSTION |
ICAS2012-6.2.3 |
Voevodenko, N. V. |
NUMERICAL RESEARCH OF THE
AIR INTAKE LOCATION INFLUENCE ONTO THE HIGH-SPEED AIRCRAFT PERFORMANCE |
ICAS2012-P2.1 |
Vogel, M. |
INVESTIGATING THE SAFETY
IMPACT OF TIME BUFFERS IN CURRENT TMA ARRIVAL OPERATIONS |
ICAS2012-9.4.3 |
Voges, V. |
APPLICATION AND POTENTIALS
OF WIRELESS COMMUNICATION TECHNOLOGIES IN PASSENGER AIR TRANSPORT FROM AN
AVIATION SECURITY STANDPOINT |
ICAS2012-9.6.3 |
Voggenreiter, H. |
NUMERICAL SIMULATIONS AND
EXPERIMENTAL INVESTIGATIONS ON QUASI-STATIC AND CYCLIC MIXED MODE
DELAMINATION OF MULTIDIRECTIONAL CFRP LAMINATES |
ICAS2012-7.4.2 |
Vörsmann, P. |
OPTIMIZATION OF A NEW
MULTI-PURPOSE UAS FOR SCIENTIFIC APPLICATIONS USING AERODYNAMIC
RECONFIGURATION |
ICAS2012-11.6.4 |
Vos, J. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
Vos, R. |
A CONCEPTUAL DESIGN AND
ANALYSIS TOOL FOR BLENDED WING BODY AIRCRAFT |
ICAS2012-1.7.2 |
Voyevodin, A. V. |
EXPERIMENTAL AND NUMERICAL
INVESTIGATIONS OF LOCAL AERODYNAMICS OF CIVIL AIRCRAFT |
ICAS2012-2.9.4 |
Vrchota, P. |
WIND TUNNEL AND CFD STUDY OF
AIRFOIL WITH AIRBRAKE |
ICAS2012-10.6.ST1 |
Vrchota, P. |
GLOBAL OPTIMIZATION OF
TWO-DIMENSIONAL HIGH LIFT AERODYNAMIC SYSTEM |
ICAS2012-11.10.2 |
Vu, N. A. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
Vuletich, I. |
APPLICATION OF THE RANGE
SAFETY TEMPLATE TOOLKIT TO UAS RISK HAZARD ANALYSES SUPPORTING AIRWORTHINESS
REGULATION |
ICAS2012-9.2.3 |
Wadia, A. R. |
THE EFFECT OF PLASMA
ACTUATORS ON TIP CLEARANCE FLOWS IN COMPRESSOR ROTORS |
ICAS2012-4.4.1 |
Wadsley, B. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
Wagner, M. |
MULTIDISCIPLINARY AIRFRAME
DESIGN OPTIMIZATION |
ICAS2012-0.4 |
Wainwright, A. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
Waitman, S. |
AUTOPILOT
DESIGN FOR THE EOLE DEMONSTRATOR |
ICAS2012-5.3.4 |
Walker, R. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
Wan, T. |
AERODYNAMIC
ANALYSIS OF 3-D FLAPPING WING MOTION VIA THE HILBERT-HUANG TRANSFORM METHOD |
ICAS2012-9.8.ST |
Wang, B. |
STUDY ON THE FLOW STRUCTURES
OF THE SHOCKWAVE AND TURBULENT BOUNDARY-LAYER INTERACTION |
ICAS2012-11.4.3 |
Wang, B. |
NUMERICAL SIMULATIONS OF
SELF-SUSTAINED AEROELASTIC OSCILLATIONS AT LOW REYNOLDS NUMBERS |
ICAS2012-2.6.3 |
Wang, B. |
SIZE EFFECT OF FAILURE MODES
IN COMPOSITE LAMINATES UNDER COMPRESSION |
ICAS2012-7.4.3 |
Wang, B. |
POST-BUCKLING
BEHAVIOR OF LAMINATED STRINGER STIFFENED PANEL UNDER COMPRESSIVE
LOAD—EXPERIMENTS AND ANALYSIS |
ICAS2012-7.4.4 |
Wang, C. |
STEADY
AND UNSTEADY FLOWS PAST AIRFOILS AT LOW REYNOLDS NUMBERS IN THE PROXIMITY OF
THE GROUND |
ICAS2012-3.6.ST |
Wang, C. H. |
EFFECT OF OFF-NORMAL LOADING
ON THE BOND STRENGTH MEASUREMENT OF BONDED REPAIRS |
ICAS2012-12.2.1 |
Wang, C. H. |
CRITICAL ASSESSMENT OF
FAILURE CRITERION FOR ADHESIVELY BONDED COMPOSITE JOINT REPAIR DESIGN |
ICAS2012-12.2.2 |
Wang, C. H. |
DELAMINATION TOUGHENING OF
CARBON-EPOXY LAMINATE WITH A POLYETHYLENE-CO-METHACRYLIC ACID (EMAA)
SELF-HEALING MODIFIER |
ICAS2012-7.6.2 |
Wang, C. H. |
INVESTIGATION INTO OPTIMISED
COMPOSITE SCARF REPAIRS WITH PRACTICAL CONSTRAINTS |
ICAS2012-P3.4 |
Wang, H. J. |
AERODYNAMIC
DESIGN OF PROPELLER FOR LONG ENDURANCE |
ICAS2012-4.5.3 |
Wang, H. S. |
STRUCTURAL
INTEGRITY ANALYSIS AND TEST OF FATIGUE CRITICAL LOCATION OF MA60 REGIONAL JET |
ICAS2012-7.9.4 |
Wang, J. |
ANALYZING AND MODELING OF
JAMMING DESTROY FACTOR |
ICAS2012-P6.1 |
Wang, J. J. |
THE DYNAMIC BEHAVIOR OF
FUNCTIONALLY GRADED PLATES UNDER THE IMPACT LOADING |
ICAS2012-7.7.3 |
Wang, L. J. |
INVESTIGATION IN THE DYNAMIC
FORCE EQUALIZATION OF DISSIMILAR REDUNDANT ACTUATION SYSTEMS OPERATING IN
ACTIVE/ACTIVE MODE |
ICAS2012-6.8.1 |
Wang, Z. |
PREDICTING NOISE EXPOSURE
FOR FLIGHT CREW MEMBERS |
ICAS2012-7.10.5 |
Watanabe, S. |
NUMERICAL STUDY OF THE
EFFECTS OF CROSS-WIND ON THE JET BLAST DEFORMATION |
ICAS2012-10.10.3 |
Watanabe, Y. |
SIMULTANEOUS OPTIMIZATION OF
AIRFRAME AND ENGINE FOR SUPERSONIC TRANSPORT |
ICAS2012-12.3.4 |
Watanabe, Y. |
EXPERIMENTAL STUDY OF
SUPERSONIC INLET FOR SUPPRESSION OF BUZZ IN SUBCRITICAL OPERATION |
ICAS2012-6.2.1 |
Watanabe, Y. |
PERFORMANCE EVALUATION OF A
BOUNDARY-LAYER DIVERTER FOR SUPERSONIC PROPULSION SYSTEM |
ICAS2012-6.2.2 |
Waterhouse, J. R. |
THE INFLUENCE OF DEMOISELLE
AIRCRAFT ON LIGHT AND GENERAL AVIATION DESIGN |
ICAS2012-1.7.ST |
Watkins, S. |
THE INFLUENCE OF TURBULENCE
INTENSITY ON THE FLOW STRUCTURE OVER A THIN AIRFOIL AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.2 |
Watkins, S. |
OPTIMUM LOCATION OF PRESSURE
MEASUREMENTS AROUND A WING AS A DYNAMIC CONTROL INPUT IN SMOOTH AND TURBULENT
CONDITIONS |
ICAS2012-3.3.3 |
Watkins, S. |
FLOW-INDUCED FLUTTER OF
SLENDER CANTILEVER HIGH-COMPLIANCE PLATES |
ICAS2012-8.10.5 |
Watkins, S. |
DYNAMIC SURFACE PRESSURE
MEASUREMENTS ON A FLAPPING WING IN SMOOTH AND TURBULENT FLOW |
ICAS2012-9.11.ST1 |
Watmuff, J. |
THE INFLUENCE OF TURBULENCE
INTENSITY ON THE FLOW STRUCTURE OVER A THIN AIRFOIL AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.2 |
Watmuff, J. |
DYNAMIC SURFACE PRESSURE
MEASUREMENTS ON A FLAPPING WING IN SMOOTH AND TURBULENT FLOW |
ICAS2012-9.11.ST1 |
Wei, A. K. L. |
CONCEPTUAL DESIGN AND
AERODYNAMIC STUDY OF BLENDED WING BODY BUSINESS JET |
ICAS2012-2.9.2 |
Wei, Y. |
SIZE EFFECT OF FAILURE MODES
IN COMPOSITE LAMINATES UNDER COMPRESSION |
ICAS2012-7.4.3 |
Weinerfelt, P. |
A COUPLED AERO AND
STRUCTURAL DYNAMICS MODEL FOR COMPUTATION OF UNSTEADY LOADS ON THE HELICOPTER
SKELDAR V200 |
ICAS2012-8.7.2 |
Weiss, M. |
TECHNOLOGY ASSESSMENT OF
FUTURE AIRCRAFT: SOCIO-ECO-EFFICIENCY IN CONCEPTUAL AIRCRAFT DESIGN |
ICAS2012-1.9.2 |
Wentink, M. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
Westphal, J. |
OPERATIONAL
HUMAN-IN-THE-LOOP INTEGRATION OF 4D ARRIVAL GUIDANCE |
ICAS2012-5.8.1 |
Wheatley, B. J. |
TUNABLE DIODE LASER
ABSORPTION SPECTROSCOPY OF HYPERSONIC FLOWS |
ICAS2012-4.8.2 |
Wheatley, V. |
THERMAL NON-EQUILIBRIUM
EFFECTS IN RADICAL FARMING SCRAMJETS |
ICAS2012-11.4.1 |
Wheatley, V. |
STREAMWISE PORTHOLE FUEL
INJECTION FOR BOUNDARY-LAYER COMBUSTION INSIDE A SCRAMJET ENGINE |
ICAS 2012-P4.16 |
Wheatley, V. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
White, B. |
MULTIPLE UAV FORMATION
RECONFIGURATION WITH COLLISION AVOIDANCE GUIDANCE VIA DIFFERENTIAL GEOMETRY
CONCEPT |
ICAS2012-11.2.2 |
Wiart, L. |
AUTOMATED CHAIN FOR
AERODYNAMIC COMPUTATIONS MEETING AIRCRAFT TRIMMING REQUIREMENTS |
ICAS2012-2.10.1 |
Wicke, K. |
MISSION AND ECONOMIC
ANALYSIS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY |
ICAS2012-1.7.4 |
Wickramasinghe, N. K. |
FLIGHT TRAJECTORY
OPTIMIZATION FOR AN EFFICIENT AIR TRANSPORTATION SYSTEM |
ICAS2012-5.8.3 |
Widjanarko, S. M. D. |
EXPERIMENTAL/NUMERICAL
INVESTIGATION AIRFOIL WITH FLOW CONTROL BY SYNTHETIC JETS |
ICAS2012-3.7.5 |
Wieczorek, K. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
Wiedemann, M. |
SENSOR AND
REAL-TIME-PROCESS-SIMULATION GUIDED AUTOCLAVE PROCESS CONTROL FOR COMPOSITE
PRODUCTION |
ICAS2012-6.1.2 |
Wild, G. |
ACOUSTIC
POWER AND DATA FOR MORE ROBUST FLIGHT DATA AND COCKPIT VOICE RECORDERS |
ICAS2012-6.10.5 |
Wild, G. |
DISTRIBUTED
OPTICAL FIBRE SMART SENSORS FOR ADVANCE SENSING SYSTEMS IN AEROSPACE VEHICLES |
ICAS2012-P6.7 |
Williams, B. |
COMPUTATIONAL ASPECTS OF
PROBABILISTIC ASSESSMENT OF UAS ROBUST AUTONOMY |
ICAS2012-9.2.2 |
Williams, B. |
EVALUATION OF ROBUST
AUTONOMY AND IMPLICATIONS ON UAS DESIGN |
ICAS2012-9.4.2 |
Williams, P. |
ALL-SOURCE NAVIGATION FOR
ENHANCING UAV OPERATIONS IN GPS-DENIED ENVIRONMENTS |
ICAS2012-11.6.1 |
Williams, P. |
INTELLIGENT LANDING SYSTEM
FOR LANDING UAVS AT UNSURVEYED AIRFIELDS |
ICAS2012-11.6.2 |
Williams, W. |
APPLICATION OF THE RANGE
SAFETY TEMPLATE TOOLKIT TO UAS RISK HAZARD ANALYSES SUPPORTING AIRWORTHINESS
REGULATION |
ICAS2012-9.2.3 |
Wilson, M. |
GROUND-BASED SENSE AND AVOID
SUPPORT FOR UNMANNED AIRCRAFT SYSTEMS |
ICAS2012-11.3.3 |
Wilson, M. |
THE SMART SKIES PROJECT:
ENABLING TECHNOLOGIES FOR FUTURE AIRSPACE ENVIRONMENTS |
ICAS2012-6.9.2 |
Wilson, S. |
APPLICATION OF THE RANGE
SAFETY TEMPLATE TOOLKIT TO UAS RISK HAZARD ANALYSES SUPPORTING AIRWORTHINESS
REGULATION |
ICAS2012-9.2.3 |
Winship, S. |
FIRE-X
407 DEVELOPMENT: UNMANNING THE BELL HELICOPTER 407 WITH THE US NAVY FIRE
SCOUT MQ-8B AUTONOMOUS SYSTEM |
ICAS2012-P1.1 |
Witte, P. |
A NON-WEIGHT BASED,
MANUFACTURING INFLUENCED DESIGN (MIND) METHODOLOGY FOR PRELIMINARY DESIGN |
ICAS2012-6.4.3 |
Wolters, F. |
IMPACT OF ALTERNATIVE FUELS
ON ENGINE PERFORMANCE AND CO2-EMISSIONS |
ICAS2012-8.6.3 |
Won, D. -Y. |
HIDDEN MARKOV MODEL
PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
ICAS2012-P6.5 |
Wong, A. K. |
MAKING THE INVISIBLE
VISIBLE: JOINING THE DOTS FROM LORD KELVIN TO FIGHTER JET FATIGUE |
ICAS2012-8.2.3 |
Wong, K. C. |
INVESTIGATION OF LOW THRUST
TO WEIGHT RATIO ROTATIONAL CAPACITY OF ASYMMETRIC MONO-WING CONFIGURATIONS |
ICAS2012-1.4.3 |
Wong, K. C. |
DESIGN AND TEST OF A UAV
BLENDED WING BODY CONFIGURATION |
ICAS2012-1.8.3 |
Worotynska, J. |
AEROELASTIC RESPONSE OF A
CHORDWISE FLEXIBLE WINGS SUBJECTED TO GUSTS: AN INITIAL STUDY ON EXPERIMENTAL
AND COMPUTATIONAL VALIDATION |
ICAS2012-8.5.3 |
Wright, L. M. |
DEVELOPMENT OF AN
EXPERIMENTAL TECHNIQUE FOR HIGH TEMPERATURE IMPINGEMENT STUDIES |
ICAS2012-12.6.3 |
Wroblewski, W. |
A HIGHLY EXPANDABLE LOW-COST
OPEN-SOURCE UAV SYSTEM WITH HIGH ON-BOARD PROCESSING POWER |
ICAS2012-1.8.1 |
Wu, S.-C. |
PILOT CONVECTIVE WEATHER
DECISION MAKING IN EN ROUTE AIRSPACE |
ICAS2012-10.4.3 |
Wu, X. R. |
ANALYSIS OF MULTIPLE SITE
DAMAGE IN AIRCRAFT STRUCTURES BY USING WEIGHT FUNCTION METHOD IN FRACTURE
MECHANICS |
ICAS2012-7.1.1 |
Wu, X. R. |
LCF BEHAVIOR AND LIFE
EVALUATION OF A SINGLE CRYSTAL NICKEL BASE SUPERALLOY UNDER DIFFERENT DWELL
CONDITION |
ICAS2012-7.3.3 |
Xia, L. |
IMPROVED PARTICLE SWARM
OPTIMIZATION BASED ON SOCIAL MODEL FOR AERODYNAMIC DESIGN |
ICAS2012-11.10.4 |
Xia, M. |
NUMERICAL STUDY OF PITCHING
OSCILLATION EFFECT ON AERODYNAMIC CHARACTERISTICS OVER ASYMMETRIC VORTEX
STRUCTURE OF SLENDER REVOLUTION |
ICAS2012-2.5.2 |
Xia, Z. F. |
TIME-ACCURATE VERSUS
ACTUATOR DISK SIMULATIONS OF PROPELLER SLIPSTREAM FLOWS |
ICAS2012-9.8.2 |
Xiao, J. |
CONTROL-ORIENTED MODELING
AND ANALYSIS OF AERO-THERMO-ELASTIC-PROPULSION HYPERSONIC VEHICLE |
ICAS2012-1.5.1 |
Xiao, Z.. X. |
INVESTIGATION OF PASSIVE
FLOW CONTROL METHODOLOGIES USING SST-IDDES |
ICAS2012-P2.7 |
Xiong, C. |
CRACK NUCLEATION MODELING IN
NOTCHED SPECIMEN SUBJECTED TO HIGH FATIGUE LOADING |
ICAS2012-7.7.4 |
Xiong, Q. |
THE WORKFLOW CONSTRUCTION
AND MANAGEMENT IN AERONAUTICAL MULTIDISCIPLINARY OPTIMIZATION |
ICAS2012-2.1.2 |
Xiong, Q. |
THE METHOD FOR NONLINEAR
ANALYSIS OPTIMIZATION IN AERONAUTICAL RESEARCH |
ICAS2012-P1.2 |
Xiong, W. |
POST-BUCKLING
BEHAVIOR OF LAMINATED STRINGER STIFFENED PANEL UNDER COMPRESSIVE
LOAD—EXPERIMENTS AND ANALYSIS |
ICAS2012-7.4.4 |
Xu, F. |
SIZE EFFECT OF FAILURE MODES
IN COMPOSITE LAMINATES UNDER COMPRESSION |
ICAS2012-7.4.3 |
Xu, G. Q. |
STUDY OF THE PRESSURE DROP
FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
ICAS2012-4.4.ST |
Xu, R. F. |
MULTI-OBJECTIVE AERODYNAMIC
OPTIMIZATION DESIGN OF MULTI-ELEMENT AIRFOIL USING KRIGING MODEL |
ICAS2012-2.3.ST |
Xu, W. |
ANALYSIS OF MULTIPLE SITE
DAMAGE IN AIRCRAFT STRUCTURES BY USING WEIGHT FUNCTION METHOD IN FRACTURE
MECHANICS |
ICAS2012-7.1.1 |
Xu, X. W. |
RESEARCH ON METHODS OF
DYNAMIC MODELING AND SIMULATION FOR MORPHING WING AIRCRAFT |
ICAS2012-5.10.ST |
Xu, Y. |
JET
NOISE REDUCTION BY MICROJETS |
ICAS2012-P4.2 |
Xue, J. |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
Xue, P. |
NUMERICAL
SIMULATION OF BIRD-STRIKING PROCESS AND ITS EXPERIMENTAL VERIFICATION |
ICAS2012-8.9.4 |
Yadlin, Y. |
HIGH-LIFT SYSTEMS FOR
ENHANCED TAKEOFF PERFORMANCE |
ICAS2012-9.5.1 |
Yakimenko, O. A. |
EXTENDING AUTONOMY
CAPABILITIES FOR UNMANNED SYSTEMS WITH CRUSER |
ICAS2012-11.6.3 |
Yakushev, V. |
METHODS AND FACILITIES TO BE
USED TO EVALUATE THE AIRCRAFT FLIGHT AND NAVIGATION EQUIPMENT IN FLIGHT TESTS |
ICAS2012-5.6.3 |
Yamada, G. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
Yamada, T. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
Yamamoto, I. |
DEVELOPMENT OF OBSERVATIONAL
SYSTEM WITH UNMANNED FLIGHT SYSTEM |
ICAS2012-P5.10 |
Yamamoto, K. |
COMPUTATIONAL STUDY ON NOISE
GENERATION FROM A TWO-WHEEL MAIN LANDING GEAR |
ICAS2012-3.9.3 |
Yamashita, Y. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
Yan, S. W. |
STUDY
ON MODELING PILOT BEHAVIOR BY ARTIFICIAL NEURAL NETWORK |
ICAS2012-5.9.ST |
Yan, W. -Y. |
NUMERICAL STUDY ON RESIDUAL
THERMAL STRESSES IN CARBON FIBRE PULLOUT |
ICAS2012-7.3.1 |
Yana, J. F. M |
PERFORMANCE ANALYSIS OF A
COAXIAL ROTOR SYSTEM IN HOVER: THREE POINTS OF VIEW |
ICAS2012-2.7.4 |
Yanagida, A. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
Yang, H. |
LAMINAR FLOW WING’S
OPTIMIZATION DESIGN BY RANS SOLVER WITH AUTOMATIC TRANSITION PREDICTION |
ICAS2012-2.2.3 |
Yang, J. |
POST-BUCKLING
BEHAVIOR OF LAMINATED STRINGER STIFFENED PANEL UNDER COMPRESSIVE
LOAD—EXPERIMENTS AND ANALYSIS |
ICAS2012-7.4.4 |
Yang, Q. |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
Yang, S. P. |
ANALYSIS
OF FLUCTUATING LOAD OF A CIRCULAR CYLINDER UNDER THE FUSELAGE |
ICAS2012-P2.17 |
Yang, S. -P. |
A PRELIMINARY CFD
INVESTIGATION ON REAR FUSELAGE SUPPORT CORRECTION |
ICAS2012-P2.14 |
Yang, X. |
EXTRACTING DECK TREND TO
PLAN DESCENT TRAJECTORY FOR SAFE LANDING OF UAVS |
ICAS2012-11.8.3 |
Yang, X. G. |
DETERMINATION OF AIRBORNE
RECORDED PARAMETERS FOR COMPREHENSIVE FLIGHT DATA MONITORING PROGRAM |
ICAS2012-9.4.1 |
Yang, Y. |
INFLUENCE OF FLAPPING WING
UNSTEADY MOTION ON AERODYNAMIC PERFORMANCE OF HORIZONTAL TAIL |
ICAS2012-2.7.5 |
Yang, Y. |
PROPELLER INDUCED GROUND
VORTEX |
ICAS2012-4.10.3 |
Yang, Y. |
TIME-ACCURATE VERSUS
ACTUATOR DISK SIMULATIONS OF PROPELLER SLIPSTREAM FLOWS |
ICAS2012-9.8.2 |
Yanovskiy, L. S. |
FUEL CELLS ON ALTERNATIVE
NON – OIL FUELS FOR GAS TURBINE ENGINES OF AN ADVANCED CIVIL AIRCRAFTS |
ICAS2012-P4.14 |
Yao, Z. X. |
RESEARCH ON OPTIMIZING
ASCENT TRAJECTORY OF AERO-SPACE PLANE BASED ON COMBINED CYCLE PROPULSION |
ICAS2012-5.7.1 |
Yarlagadda, P. |
A MICRO-SIMULATION OF
AIRPORT PASSENGERS WITH ADVANCED TRAITS |
ICAS2012-10.9.4 |
Yashin, Y. P. |
EFFECTS OF MANIPULATOR TYPE
AND FEEL SYSTEM CHARACTERISTICS ON HIGH-FREQUENCY BIODYNAMIC PILOT-AIRCRAFT
INTERACTION |
ICAS2012-5.9.3 |
Yashin, Y. P. |
SOME ASPECTS OF MOVING-BASE
SIMULATION OF UPSET RECOVERING MANEUVER |
ICAS2012-5.9.4 |
Yeo, E. |
EFFECT OF OFF-NORMAL LOADING
ON THE BOND STRENGTH MEASUREMENT OF BONDED REPAIRS |
ICAS2012-12.2.1 |
Yi, J. J. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
Yokokawa, Y. |
COMPUTATIONAL STUDY ON NOISE
GENERATION FROM A TWO-WHEEL MAIN LANDING GEAR |
ICAS2012-3.9.3 |
Yokozeki, T. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
Yoo, D. -W. |
CONTROLLER DESIGN AND
ANALYSIS OF UNMANNED AERIAL VEHICLES USING AUTOMATIC GAIN GENERATION
TECHNIQUE |
ICAS2012-11.8.1 |
Yoo, S. -J. |
AEROELASTIC ANALYSIS FOR
HELICOPTER ROTOR BLADES IN HOVER AND FORWARD FLIGHTS |
ICAS2012-11.5.3 |
Yoshida, K. |
D-SEND PROJECT FOR LOW SONIC
BOOM DESIGN TECHNOLOGY |
ICAS2012-1.2.1 |
Yoshida, K. |
DEVELOPMENT OF SUPERSONIC
NATURAL LAMINAR FLOW WING DESIGN SYSTEM USING CFD-BASED INVERSE METHOD |
ICAS2012-2.2.1 |
Yoshida, K. |
STABILITY ANALYSIS ON
NATURAL LAMINAR FLOW WING IN SUPERSONIC FLOW: ONERA-JAXA JOINT RESEARCH
PROGRAM |
ICAS2012-3.10.1 |
Yoshida, K. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
Yoshida, Y. |
INTEGRATED DESIGN METHOD OF
A ROCKET ENGINE TURBOPUMP SUB-SYSTEM FOR SUPPRESSING ROTOR LATERAL VIBRATION |
ICAS2012-4.3.4 |
Yoshihara, T. |
GBAS CURVED APPROACH
PROCEDURES: ADVANTAGES, CHALLENGES AND APPLICABILITY |
ICAS2012-4.9.2 |
You, J. H. |
AEROACOUSTIC ANALYSIS OF A
HELICOPTER CONFIGURATION WITH DUCTED TAIL ROTOR |
ICAS2012-3.9.1 |
Young, T. M. |
EVALUATION AND CORRELATION
OF INTER-LABORATORY RESULTS FROM A RAIN EROSION TEST CAMPAIGN |
ICAS2012-12.2.3 |
Young, T. M. |
LABORATORY TESTING OF INSECT
CONTAMINATION FOR LAMINAR FLOW APPLICATIONS USING AN INSECT-IMPACT TEST
FACILITY |
ICAS2012-3.4.4 |
Yu, H. C. |
LCF BEHAVIOR AND LIFE
EVALUATION OF A SINGLE CRYSTAL NICKEL BASE SUPERALLOY UNDER DIFFERENT DWELL
CONDITION |
ICAS2012-7.3.3 |
Yu, J. G. |
FLOW
CONTROL TEST RESEARCH OF AIRCRAFT MODEL WITH ADJUSTABLE CANAEDS |
ICAS2012-P2.5 |
Yu, M. S. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
Yu, X. |
STUDY OF THE PRESSURE DROP
FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
ICAS2012-4.4.ST |
Yu, X. |
LOAD SYNTHESIS OF HELICOPTER
DYNAMIC COMPONENTS: IMPROVEMENTS TO LINEAR REGRESSION IN THE AZIMUTH DOMAIN |
ICAS2012-8.10.ST |
Yuan, W. |
DESIGN OF A mu SYNTHESIS
CONTROLLER TO STABILIZE AN UNMANNED HELICOPTER |
ICAS2012-11.5.2 |
Yuan, W. |
A GREY-BOX SYSTEM
IDENTIFICATION PROCEDURE FOR SCALE MODEL HELICOPTERS BASED ON
FREQUENCY-DOMAIN ESTIMATION METHODS |
ICAS2012-11.9.ST |
Yuan, W. |
NUMERICAL SIMULATIONS OF
SELF-SUSTAINED AEROELASTIC OSCILLATIONS AT LOW REYNOLDS NUMBERS |
ICAS2012-2.6.3 |
Yuhara, T. |
CONCEPTUAL DESIGN STUDY ON
LOW BOOM LH2 SUPERSONIC TRANSPORT -
CONSIDERING CLIMATE CHANGE IMPACT |
ICAS2012-1.2.3 |
Yulong, L. |
THE
NUMERICAL SIMULATION OF BIRD STRIKE ON BLADES OF AN ENGINE |
ICAS2012-4.4.3 |
Zaichik, L. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
Zaichik, L. E. |
EFFECTS OF MANIPULATOR TYPE
AND FEEL SYSTEM CHARACTERISTICS ON HIGH-FREQUENCY BIODYNAMIC PILOT-AIRCRAFT
INTERACTION |
ICAS2012-5.9.3 |
Zaichik, L. E. |
SOME ASPECTS OF MOVING-BASE
SIMULATION OF UPSET RECOVERING MANEUVER |
ICAS2012-5.9.4 |
Zammit-Mangion, D. |
A CASE STUDY OF ARRIVAL AND
DEPARTURE MANAGERS COOPERATION FOR REDUCING AIRBORNE HOLDING TIMES AT
DESTINATION AIRPORTS |
ICAS2012-10.1.ST |
Zammit-Mangion, D. |
A PROPOSAL FOR REVISED
APPROACHES AND PROCEDURES TO MALTA INTERNATIONAL AIRPORT |
ICAS2012-4.9.3 |
Zammit-Mangion, D. |
TOWARDS TRAJECTORY
PREDICTION AND OPTIMISATION FOR ENERGY EFFICIENCY OF AN AIRCRAFT WITH
ELECTRICAL AND HYDRAULIC ACTUATION SYSTEMS |
ICAS2012-6.7.3 |
Zammit-Mangion, D. |
CORRESPONDENCE AND
CLUSTERING METHODS FOR IMAGE-BASED WING-TIP COLLISION AVOIDANCE TECHNIQUES |
ICAS2012-9.10.4 |
Zammit-Mangion, D. |
BI-OBJECTIVE PSEUDOSPECTRAL
OPTIMAL CONTROL TECHNIQUES FOR AIRCRAFT TRAJECTORY OPTIMIZATION |
ICAS2012-P5.6 |
Zapotezny-Anderson, P. M. |
DESIGN OF FLIGHT AVOIDANCE
MANOEUVRE ALPHABETS FOR MIXED CENTRALISED-DECENTRALISED SEPARATION MANAGEMENT |
ICAS2012-10.7.3 |
Zare-Behtash, H. |
PERFORMANCE ANALYSIS OF A
SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
ICAS2012-P4.12 |
Zeng, Z. |
FLEXIBLE WING AERODYNAMICS
AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.1 |
Zhang, B. |
FRACTURE
ANALYSIS OF BLADE DOVETAIL OF TC11 TITANIUM ALLOY |
ICAS2012-P4.7 |
Zhang, J. J. |
THE STUDY ON THE AIRCRAFT
INTEGRATED CHARACTERS WITH DIFFERENT HEIGHT WINGLETS |
ICAS2012-P2.9 |
Zhang, K. |
LAMINAR FLOW WING’S
OPTIMIZATION DESIGN BY RANS SOLVER WITH AUTOMATIC TRANSITION PREDICTION |
ICAS2012-2.2.3 |
Zhang, K. -S |
DESIGN OF LAMINAR
SUPERCRITICAL AIRFOILS BASED ON NAVIER-STOKES EQUATIONS |
ICAS2012-2.2.2 |
Zhang, K. -S. |
MULTIDISCIPLINARY EVALUATION
OF TRUSS-BRACED WING FOR FUTURE GREEN AIRCRAFT |
ICAS2012-1.10.ST |
Zhang, R. |
THE WORKFLOW CONSTRUCTION
AND MANAGEMENT IN AERONAUTICAL MULTIDISCIPLINARY OPTIMIZATION |
ICAS2012-2.1.2 |
Zhang, R. |
A GENERAL FOOTPRINT
GENERATION APPROACH FOR LIFTING RE-ENTRY VEHICLE |
ICAS2012-5.7.2 |
Zhang, R. |
ANGLE OF ATTACK OPERATION
ZONE ANALYSIS AND DESIGN FOR LIFTING ENTRY |
ICAS2012-5.7.3 |
Zhang, R. |
A NEW APPROACH FOR RE-ENTRY
VEHICLE TRAJECTORY PLANNING AND GUIDANCE |
ICAS2012-5.7.5 |
Zhang, R. |
THE METHOD FOR NONLINEAR
ANALYSIS OPTIMIZATION IN AERONAUTICAL RESEARCH |
ICAS2012-P1.2 |
Zhang, S. C. |
LCF BEHAVIOR AND LIFE
EVALUATION OF A SINGLE CRYSTAL NICKEL BASE SUPERALLOY UNDER DIFFERENT DWELL
CONDITION |
ICAS2012-7.3.3 |
Zhang, T. |
RESEARCH ON CRACK GROWTH OF
MULTIPLE-SITE DAMAGED STRUCTURE |
ICAS2012-7.1.3 |
Zhang, W. |
RESEARCH ON METHODS OF
DYNAMIC MODELING AND SIMULATION FOR MORPHING WING AIRCRAFT |
ICAS2012-5.10.ST |
Zhang, W. |
THE GLARE EVALUATION METHOD
FOR CIVIL AIRPLANE FLIGHT DECK |
ICAS2012-9.3.3 |
Zhang, W. S. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
Zhang, X. |
EXTENSIONS OF MENTER’S SST
TRANSITION MODEL TO SIMULATE HYPERSONIC AND CROSS-FLOW TRANSITION |
ICAS2012-11.4.ST |
Zhang, X. |
DEVELOPMENT
OF THE OPTIMIZED APPROACH AND LANDING TRAJECTORY FOR FUTURE AIR TRANSPORT
SYSTEM |
ICAS2012-P8.1 |
Zhang, X. Q. |
THE DYNAMIC BEHAVIOR OF
FUNCTIONALLY GRADED PLATES UNDER THE IMPACT LOADING |
ICAS2012-7.7.3 |
Zhang, Y. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
Zhang, Z. B. |
THE
INTEGRATION OPTIMIZATION DESIGN OF AERODYNAMIC AND STEALTH FOR FIGHTERS |
ICAS2012-P2.2 |
Zhang, Z. B. |
EXPERIMENTAL
INVESTIGATION OF INFRARED STEALTH TECHNOLOGIES OF AERO-ENGINE EXHAUST SYSTEM |
ICAS2012-P4.1 |
Zhang, Z.- H. |
NUMERICAL INVESTIGATION OF
FLOW OVER MULTI-ELEMENT AIRFOILS WITH LIFT-ENHANCING TABS |
ICAS2012-2.3.2 |
Zhao, K. |
CFD-BASED RESEARCH OF STRAKE
EFFECTS FOR LOW SPEED HIGH LIFT CONFIGURATION |
ICAS2012-P2.16 |
Zhao, K. |
NUMERICAL SIMULATION OF
TRANSONIC SHOCK-VORTEX INTERACTION FLOW AROUND THE VFE-2 DELTA WING BASED ON
MDDES |
ICAS2012-P2.4 |
Zhao, N. |
NUMERICAL
SIMULATION OF BIRD-STRIKING PROCESS AND ITS EXPERIMENTAL VERIFICATION |
ICAS2012-8.9.4 |
Zhao, W. |
STUDIES ON IMPROVEMENT OF
NONLINEAR PITCHING MOMENT CHARACTERISTICS OF CRANKED-ARROW WING |
ICAS2012-3.2.1 |
Zhao, Y. |
STUDY ON THE FLOW STRUCTURES
OF THE SHOCKWAVE AND TURBULENT BOUNDARY-LAYER INTERACTION |
ICAS2012-11.4.3 |
Zheng, X. |
ON
THE KNEE-POINT PHENOMENON IN COMPOSITE LAMINATES UNDER LOW-VELOCITY IMPACT
AND QUASI-STATIC INDENTATION |
ICAS2012-7.7.ST |
Zhong, B. |
EXTENSIONS OF MENTER’S SST
TRANSITION MODEL TO SIMULATE HYPERSONIC AND CROSS-FLOW TRANSITION |
ICAS2012-11.4.ST |
Zhong, Y. |
CFD-BASED RESEARCH OF STRAKE
EFFECTS FOR LOW SPEED HIGH LIFT CONFIGURATION |
ICAS2012-P2.16 |
Zhou, H. |
DEVELOPMENT
OF THE OPTIMIZED APPROACH AND LANDING TRAJECTORY FOR FUTURE AIR TRANSPORT
SYSTEM |
ICAS2012-P8.1 |
Zhou, T. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
Zhu, J. |
APPLICATION
OF TWO TRANSITION MODELS TO FLOWS AROUND AIRFOILS |
ICAS2012-2.4.4 |
Zhu, J. J. |
THE PERFORMANCE COMPUTATION
OF THE HOT AIR ANTI-ICING SYSTEM OF AN AERO-ENGINE CONE |
ICAS2012-2.6.2 |
Zhu, K. H. |
THE GENERALIZED ARRIVAL
PLANNER (GARP): MODELING AND ANALYSIS FOR ARRIVAL PLANNING |
ICAS2012-10.9.3 |
Zhu, Y. |
ANALYZING AND MODELING OF
JAMMING DESTROY FACTOR |
ICAS2012-P6.1 |
Zhu, Z. |
LAMINAR FLOW WING’S
OPTIMIZATION DESIGN BY RANS SOLVER WITH AUTOMATIC TRANSITION PREDICTION |
ICAS2012-2.2.3 |
Zhuang, Q. |
EFFECT ON THE AERODYNAMIC
FORCING IN AN AXIAL TURBINE STAGE ON VARYING STATOR BLADE SHAPE |
ICAS2012-4.3.ST |
Zichenkov, M. |
ANALYSIS OF STATIC AND
DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW |
ICAS2012-8.10.4 |
Zietarski, S. |
A NEW APPROACH TO IDENTIFICATION AND OPTIMIZATION OF AIRFOILS
BY USING THE COMBINATORIAL-CYCLIC METHOD |
ICAS2012-P2.24 |
Zoltak, J. |
OPTIMISATION OF THE
HELICOPTER FUSELAGE WITH SIMULATION OF MAIN AND TAIL ROTOR INFLUENCE |
ICAS2012-1.4.1 |
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