Name |
Title |
ICAS Paper Number |
Abbot, T. S. |
SIMULATION RESULTS FOR AIRBORNE PRECISION SPACING ALONG CONTINUOUS DESCENT ARRIVALS |
ICAS 2008-11.9.2 (AIAA 2008-8931) |
Abdalla, A. M. |
AERO-STRUCTURAL MDO OF A SPAR-TANK-TYPE WING FOR AIRCRAFT CONCEPTUAL DESIGN |
ICAS2008-1.1 ST: |
Abdi, F. |
COHESIVE DISINTEGRATION IN IMPACTED RE-ENTRY SPACE TRANSPORTATION HYBRID STRUCTURES |
ICAS 2008-7.5.1 |
Abdi, F. |
PREDICTION OF DELAMINATION IN ADVANCED AEROSPACE COMPOSITE STRUCTURES USING MICRO/MACRO MECHANICS CONSTITUTIVE METHODS |
ICAS 2008-7.5.3 |
Abedian, A. |
AN ANALYTICAL MODEL FOR PREDICTION OF THE STEADY STATE CREEP DEFORMATIONS AND STRESSES OF SHORT FIBER COMPOSITES |
ICAS 2008-9.8.3 |
Abedian, A. |
EFFECTS OF HIERARCHY ORDER ON NATURAL FREQUENCY AND VIBRATION TRANSMISSION OF SELF-SIMILAR TRUSSES |
ICAS2008-P3.9 |
Abedian, A. |
FEM MICRO-MECHANICAL ANALYSIS OF DELAMINATION PHENOMENON IN IMC LAMINATED COMPOSITES USING DAMAGE THEORY |
ICAS2008-9.4 ST: |
Abedian, A. |
MICROMECHANICAL FEM MODELING OF THERMAL STRESSES IN FUNCTIONALLY GRADED MATERIALS |
ICAS 2008-7.2.4 |
Abedian, A. |
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF A SATELLITE BOOM STRUCTURE TO REDUCE WEIGHT AND VIBRATION TRANSMISSION USING GA |
ICAS2008-P3.8 |
Abrahamson, P. D. |
DEVELOPMENT AND APPLICATION OF AN INTEGRATED APPROACH TOWARD NASA AIRSPACE SYSTEMS RESEARCH |
ICAS 2008-10.8.1 (AIAA 2008-8924) |
Adams, N. A. |
AERODYNAMIC INVESTIGATIONS ON A GENERIC FAN-IN-WING CONFIGURATION |
ICAS 2008-3.5.1 |
Adeyefa, S. |
EVAPORATING COOLANT FOR ON-BOARD COOLING SYSTEMS WITH DIRECT CONDENSATION THROUGH AMBIENT AIR |
ICAS 2008-6.6.3 |
Adzic, M. |
ON AIRCRAFT PERFORMANCE IMPROVEMENT BY USING WINGLETS |
ICAS 2008-2.8.3 |
Ahmad, N. |
AIRSHIP TRANSPORT OPERATIONAL MANAGEMENT IN NORTHERN LATITUDES |
ICAS 2008-10.1.1 (AIAA 2008-8850) |
Airoldi, A. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
Akbarpour, S. |
MICROMECHANICAL FEM MODELING OF THERMAL STRESSES IN FUNCTIONALLY GRADED MATERIALS |
ICAS 2008-7.2.4 |
Alderliesten, R. C. |
FATIGUE CRACK GROWTH PREDICTION OF FIBRE REINFORCED METAL LAMINATES UNDER VARIABLE AMPLITUDE LOADING |
ICAS 2008-7.6.1 |
Alderliesten, R. C. |
THE INFLUENCE OF FATIGUE CRACK INITIATION BEHAVIOUR OF FRICTION STIR WELDED JOINTS ON THE DESIGN CRITERIA |
ICAS 2008-7.6.2 |
Allen, C. B. |
TOWARDS AERODYNAMIC OPTIMISATION OF AN AEROELASTIC WING USING DOMAIN ELEMENT PARAMETERISATION |
ICAS 2008-2.8.1 |
Allen, D. |
HEALTH MONITORING FOR COMMERCIAL AIRCRAFT SYSTEMS |
ICAS 2008-6.1.2 |
Allerton, D. J. |
REAL-TIME SIMULATION OF A DISTRIBUTED CONFLICT RESOLUTION ALGORITHM |
ICAS 2008-8.7.3 |
Alves, P. M. |
AVIATION TELEMEDICINE: PAST, PRESENT AND FUTURE |
ICAS 2008-9.2.2 |
Amadori, K. |
AIRCRAFT CONCEPTUAL DESIGN AUTOMATION |
ICAS 2008-1.8.1 |
Amadori, K. |
RAVEN – A SUBSCALE RADIO CONTROLLED BUSINESS JET DEMONSTRATOR |
ICAS 2008-5.5.2 |
Amelsberg, S. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
Amelsberg, S. |
GENERATION OF HIGH ACCURATE 4D TRAJECTORIES FOR TAKE-OFF AND DEPARTURE |
ICAS2008-8.11 ST: |
Amiryants, G. |
ACTIVE AEROELASTICITY CONCEPT: NOVEL VIEW, METHODOLOGY AND RESULTS |
ICAS 2008-9.6.1 INVITED |
An, G. |
THE NUMERICAL SIMULATION ANALYSIS OF KEY STRUCTURES OF INTEGRATED POWER SUPPLY IN MOTOR-PUMP |
ICAS2008-P6.2 |
An, S. J. |
UNSTEADY PROPULSIVE CHARACTERISTICS OF BIOFOILS MOVING IN A VERY LOW-REYNOLDS NUMBER FLOW |
ICAS 2008-3.9.3 |
An, W. G. |
A NEW EFFICIENT INTERACTIVE MULTI-OBJECTIVE EVOLUTIONARY OPTIMIZATION ALGORITHM AND APPLICATION IN ENGINEERING |
ICAS2008-6.2 ST: |
Anand, V. |
APPLICATION OF SHAPE OPTIMISATION TO AIRCRAFT WING STRUCTURES |
ICAS 2008-7.8.3 |
Anastasijevic, Z. |
APPLICATION OF SEMICONDUCTOR STRAIN GAUGES IN MEASUREMENTS OF DYNAMIC STABILITY DERIVATIVES IN THE T-38 WIND TUNNEL |
ICAS 2008-3.4.5 |
Andersson, H. |
HOSTED SIMULATION FOR HETEROGENEOUS AIRCRAFT SYSTEM DEVELOPMENT |
ICAS2008-6.2 ST: |
Ando, T. |
DEVELOPMENT OF AN ONBOARD DOPPLER LIDAR FOR FLIGHT SAFETY |
ICAS 2008-9.9.2 |
Anghileri, M. |
BIRDSTRIKE ONTO STRUCTURES IN ROTATIONAL MOTION |
ICAS 2008-9.4.4 |
Anghileri, M. |
SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT |
ICAS 2008-7.9.2 |
Antunes, A. P. |
AN AERODYNAMIC OPTIMIZATION FRAMEWORK BASED ON GENETIC ALGORITHMS |
ICAS 2008-2.3.4 |
Aoki, T. |
IMPACT CHARACTERISTICS ESTIMATION OF SHORT SUPPORT COLUMNS UNDER CABIN FLOOR |
ICAS 2008-9.4.1 |
Arendsen, P. |
OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION |
ICAS 2008-2.11.2 |
Arimoto, M. |
DEVELOPMENT OF THE DISPLAY DEVICE OF POWER DISTIBUTION SYSTEM (DEVELOPMENT OF THE DEPTH FUSED 3-D DISPLAY FOR AIRCRAFT) |
ICAS2008-6.5 ST: |
Arizono, H. |
TRANSONIC FLUTTER WIND TUNNEL TESTS OF CONVENTIONAL TWIN-ENGINE TRANSPORT SEMISPAN MODEL |
ICAS 2008-9.6.2 |
Armstrong, M. |
FUNCTION BASED ARCHITECTURE DESIGN SPACE DEFINITION AND EXPLORATION |
ICAS 2008-1.9.3 (AIAA 2008-8928) |
Armstrong, M. |
METHODOLOGY FOR AIRCRAFT SYSTEM ARCHITECTURE SIZING |
ICAS 2008-6.2.2 |
Asai, K. |
EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE |
ICAS 2008-3.7.5 |
Aschenbrenner, L. |
MECHANICS OF COMPOSITES IN LIGHTWEIGHT STRUCTURES: EFFICIENT TESTING AND COMPUTATION ACCOUNTING FOR COMPLEX 3D BEHAVIOUR |
ICAS 2008-7.11.2 |
Asim, M. |
FRAMEWORK OF PAKISTAN AEROSPACE INDUSTRY QUALITY SYSTEM |
ICAS 2008-6.9.4 |
Aso, S. |
AERODYNAMIC DESIGN AND ITS VALIDATION OF AN OPEN-TYPE ENGINE RUN-UP FACILITY |
ICAS 2008-4.5.3 |
Aso, S. |
CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION |
ICAS 2008-1.2.3 |
Aso, S. |
NUMERICAL STUDY OF THE EFFECT OF THE OPPOSING JET ON REDUCTION OF AERODYNAMIC HEATING WITH DIFFERENT NOSE CONFIGURATIONS |
ICAS 2008-3.6.3 |
Astarita, T. |
EXPERIMENTAL ANALYSIS OF THE FLOW FIELD IN A ROTATING 'U' CHANNEL |
ICAS 2008-4.6.3 |
Astarita, T. |
MODULATION TRANSFER FUNCTION OF STEREO PARTICLE IMAGE VELOCIMETRY TECHNIQUE |
ICAS2008-P2.6 |
Atkins, S. |
IMPLICATION OF VARIABILITY IN AIRPORT SURFACE OPERATIONS ON 4-D TRAJECTORY PLANNING |
ICAS 2008-11.11.3 (AIAA 2008-8960) |
Atkins, S. |
IMPROVED PREDICTION OF GATE DEPARTURE TIMES USING PRE-DEPARTURE EVENTS |
ICAS 2008-11.8.1 (AIAA 2008-8919) |
Atobe, T. |
LARGE EDDY SIMULATION AROUND 2-D AIRFOIL WITH NATURAL TRANSITION AT HIGH REYNOLDS NUMBERS |
ICAS2008-2.1 ST: |
Attia, M. S. |
APPLICATION OF THE INTEGRATED PRODUCT TEAM (IPT) CONCEPT TO THE RE-ENGINE OF A VERY LIGHT JET (VLJ) |
ICAS 2008-6.7.5 |
Auger, D. |
FLIGHT SIMULATORS – ON DIFFERENT PERCEPTIONS OF MANUFACTURERS, AVIATION AUTHORITIES, RESEARCH AND USERS |
ICAS 2008-5.5.1 INVITED |
Auriti, L. |
CESSNA CITATION CJ1 FLIGHT TEST DATA GATHERING AND LEVEL-C SIMULATOR MODEL DEVELOPMENT |
ICAS 2008-5.1.2 |
Aversa, N |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
Axelsson, L.-U. |
EVALUATION OF THE FLOW IN AN INTERMEDIATE TURBINE DUCT AT OFF-DESIGN CONDITIONS |
ICAS 2008-4.6.2 |
Ayuso, L. |
AERODYNAMIC OPTIMIZATION OF A BLENDED WING BODY |
ICAS2008-2.11 ST: |
Azevedo, J. L. F. |
AN AERODYNAMIC OPTIMIZATION FRAMEWORK BASED ON GENETIC ALGORITHMS |
ICAS 2008-2.3.4 |
Azevedo, J. L. F. |
APPLICATION OF A NAVIER-STOKES CODE TO THE SIMULATIONS OF HIGH-LIFT DEVICES USING UNSTRUCTURED GRIDS |
ICAS 2008-2.2.4 |
Azevedo, J. L. F. |
DYNAMIC ANALYSIS OF AEROELASTIC RESPONSE FOR TRANSONIC FLOW WITH NONLINEAR STRUCTURAL MODEL |
ICAS 2008-9.6.4 |
Badalamenti, C. |
VORTEX SHEDDING FROM A ROTATING CIRCULAR CYLINDER AT MODERATE SUB-CRITICAL REYNOLDS NUMBERS AND HIGH VELOCITY RATIO |
ICAS 2008-3.10.5 |
Badanik, B. |
AIRLINES’ POINT OF VIEW AS A NEW APPROACH TO MEASURING QUALITY OF SERVICE AT AIRPORTS |
ICAS 2008-8.3.3 |
Badiey, M. |
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF A SATELLITE BOOM STRUCTURE TO REDUCE WEIGHT AND VIBRATION TRANSMISSION USING GA |
ICAS2008-P3.8 |
Bagassi, S. |
DESIGN AND DEVELOPMENT OF AN ATC DISTRIBUTED TRAINING SYSTEM |
ICAS2008-P8.2 (AIAA 2008-8873) |
Bagassi, S. |
DESIGN AND EVALUATION OF A 4D INTERFACE FOR ATC |
ICAS 2008-9.10.3 |
Bai, J. |
SATELLITE-BASED NAVIGATION ARCHITECTURE STUDY FOR AIRCRAFT CATEGORY III LANDINGS |
ICAS 2008-6.4.4 |
Bailey, L. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
Baklanov, V. |
PROBLEMS OF VIBROACOUSTICS FOR NEW AIRPLANE GENERATION |
ICAS 2008-4.9.4 |
Balasubramanian, S. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Baldomir, A. |
SIZE OPTIMIZATION OF AIRCRAFT STRUCTURES |
ICAS2008-7.11 ST: |
Baldwin, K. |
AN AUTOMATED SIMULATION PILOT CAPABILITY TO SUPPORT ADVANCED AIR TRAFFIC CONTROLLER TRAINING |
ICAS 2008-10.5.3 (AIAA 2008-8897) |
Balzer, W. |
INVESTIGATION OF SEPARATION CONTROL FOR LOW-PRESSURE TURBINES USING CFD |
ICAS 2008-4.4.2 |
Banerjee, S. |
LOW COST TRANS-RIVER AERIAL-FERRY USING A NOVEL LTA SYSTEM |
ICAS 2008-10.1.2 (AIAA 2008-8851) |
Bansmer, S. |
A COMPARISON OF NUMERICAL RANS SIMULATIONS AND FLOW FIELD MEASUREMENTS OF AN OSCILLATING AIRFOIL FOR FLAPPING WING PROPULSION |
ICAS 2008-2.10.2 |
Barhydt, R. |
DEVELOPMENT AND APPLICATION OF AN INTEGRATED APPROACH TOWARD NASA AIRSPACE SYSTEMS RESEARCH |
ICAS 2008-10.8.1 (AIAA 2008-8924) |
Barmore, B. E. |
SIMULATION RESULTS FOR AIRBORNE PRECISION SPACING ALONG CONTINUOUS DESCENT ARRIVALS |
ICAS 2008-11.9.2 (AIAA 2008-8931) |
Barret et al, S. |
INTERDEPENDENCIES IN LOCAL AIR QUALITY AND NOISE IMPACTS FOR LANDING AND TAKEOFF OPERATIONS |
ICAS 2008-11.3.2 (AIAA 2008-8866) |
Barrett, T. |
THE QUEST FOR A TRULY PARSIMONIOUS AIRFOIL PARAMETERIZATION SCHEME |
ICAS2008-P2.2 (AIAA 2008-8879) |
Barros, P. A. |
AN APPROACH FOR VERIFICATION AND VALIDATION OF THE ENVIRONMENTAL DESIGN SPACE |
ICAS2008-P8.4 (AIAA 2008-8875) |
Basso, E. |
APPLICATION OF A NAVIER-STOKES CODE TO THE SIMULATIONS OF HIGH-LIFT DEVICES USING UNSTRUCTURED GRIDS |
ICAS 2008-2.2.4 |
Basso, N. |
INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS |
ICAS 2008-7.2.1 |
Bateman, H. L. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
Battezzato, A. |
FLY-BY-WIRE CONTROL OF A HELICOPTER: MULTIBODY MAIN ROTOR MODEL |
ICAS2008-5.11 ST: |
Battiste, V. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
Baumeister, R. |
REAL-TIME SIMULATION OF A DISTRIBUTED CONFLICT RESOLUTION ALGORITHM |
ICAS 2008-8.7.3 |
Bauschat, J.-M. |
FLIGHT SIMULATORS – ON DIFFERENT PERCEPTIONS OF MANUFACTURERS, AVIATION AUTHORITIES, RESEARCH AND USERS |
ICAS 2008-5.5.1 INVITED |
Baxley, B. T. |
SIMULATION RESULTS FOR AIRBORNE PRECISION SPACING ALONG CONTINUOUS DESCENT ARRIVALS |
ICAS 2008-11.9.2 (AIAA 2008-8931) |
Bayandor, J. |
BWB MILITARY CARGO TRANSPORT FUSELAGE DESIGN AND ANALYSIS |
ICAS 2008-7.9.3 |
Bayandor, J. |
COHESIVE DISINTEGRATION IN IMPACTED RE-ENTRY SPACE TRANSPORTATION HYBRID STRUCTURES |
ICAS 2008-7.5.1 |
Bayandor, J. |
INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS |
ICAS 2008-7.2.1 |
Bayandor, J. |
PREDICTION OF DELAMINATION IN ADVANCED AEROSPACE COMPOSITE STRUCTURES USING MICRO/MACRO MECHANICS CONSTITUTIVE METHODS |
ICAS 2008-7.5.3 |
Bayandor, J. |
THE DESIGN OF POSTBUCKLING COMPOSITE AEROSPACE STRUCTURES ACCOUNTING FOR DAMAGE INITIATION AND GROWTH |
ICAS 2008-7.3.2 |
Bazso, Z. |
CAPACITY RESEARCH OF BRNO-TURANY AIRPORT WITH RESPECT TO NEW TRENDS IN AIR TRANSPORT |
ICAS 2008-8.5.3 |
Beaton, E. |
INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.10.1 (AIAA 2008-8940) |
Beaumier, P. |
AERODYNAMIC AND AERO-ACOUSTIC DESIGN OF MODERN TILT-ROTORS: THE ONERA EXPERIENCE |
ICAS 2008-1.7.4 |
Beccaro, A. |
A NEW AIRCRAFT CONCEPT: THE COMBAT MALE |
ICAS 2008-1.4.4 |
Becker (retired), J. |
APPLICATION OF PVDF FOILS FOR THE MEASUREMENTS OF UNSTEADY PRESSURES ON WIND TUNNEL MODELS FOR THE PREDICTION OF AIRCRAFT VIBRATIONS |
ICAS 2008-3.4.2 |
Becker, G. G. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
Becker, H. |
PERFORMANCE-BASED TMA HANDLING FOR MIXED TRAFFIC USING A GROUND BASED 4D-GUIDANCE FOR UNEQUIPPED AIRCRAFT |
ICAS 2008-10.8.3 |
Beelaerts van Blokland, W. W. A. |
DESIGN OF A LEAN MRO BUSINESS PROCESS FOR EPCOR |
ICAS 2008-10.3.4 (AIAA 2008-8864) |
Benedictus, R. |
FATIGUE CRACK GROWTH PREDICTION OF FIBRE REINFORCED METAL LAMINATES UNDER VARIABLE AMPLITUDE LOADING |
ICAS 2008-7.6.1 |
Benedictus, R. |
THE INFLUENCE OF FATIGUE CRACK INITIATION BEHAVIOUR OF FRICTION STIR WELDED JOINTS ON THE DESIGN CRITERIA |
ICAS 2008-7.6.2 |
Benmeddour, A. |
TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT |
ICAS 2008-2.9.2 |
Bérard, A. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
Bérard, A. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
Berard, C. |
MODELLING OF THE 3-DOF NONLINEAR AIRCRAFT BEHAVIOUR VIA SMALL STANDARD FORMS |
ICAS2008-P5.5 |
Berends, J. P. T. J. |
MDO DESIGN SUPPORT BY INTEGRATED ENGINEERING SERVICES WITHIN A MULTI-AGENT TASK ENVIRONMENT |
ICAS 2008-1.11.1 (AIAA 2008-8947) |
Berezin, A. V. |
ESTIMATION OF CRACK TURN PHENOMENON |
ICAS 2008-7.6.3 |
Berge et al, M. |
COLLABORATIVE FLOW MANAGEMENT: ANALYSIS OF BENEFITS DURING CONVECTIVE WEATHER DISRUPTIONS |
ICAS 2008-11.7.5 (AIAA 2008-8911) |
Berge, M. |
ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES |
ICAS 2008-11.9.3 (AIAA 2008-8932) |
Bergsma, O. K. |
CARBON/DYNEEMA INTRALAMINAR HYBRIDS: NEW STRATEGY TO INCREASE IMPACT RESISTANCE OR DECREASE MASS OF CARBON FIBER COMPOSITES |
ICAS 2008-7.3.4 |
Berth, C. |
RESEARCH ON INTEGRATED COLLIMATED COCKPIT VISUAL AND FLIGHT INFORMATION SYSTEM |
ICAS 2008-9.10.1 |
Bertini, F. |
EULER INVERSE THROUGHFLOW MODEL BASED ON AN IMPLICIT UPWIND TIME MARCHING TECHNIQUE |
ICAS 2008-2.3.2 |
Berton, B. |
A NOVEL RECIPROCAL SOUND TRANSMISSION MEASURING METHOD, APPLIED ON A COMPOSITE FUSELAGE |
ICAS 2008-4.9.3 |
Bes, C. |
CAPACITY MODELLING FOR FUTURE AERONAUTICAL SAFETY COMMUNICATIONS OVER WIDE AREAS |
ICAS 2008-8.8.2 (AIAA 2008-8952) |
Bettini, P. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
Beyers, M. E. |
COMPUTATIONAL FLUID DYNAMICS AND EXPERIMENTAL INVESTIGATION OF AIRPLANE STALL DYNAMICS WITH WING CONTAMINATION |
ICAS 2008-3.5.2 |
Bhadra, D. |
IMPACT OF US-EU OPEN AREA AVIATION TREATY ON US AVIATION: A PARAMETRIC ANALYSIS WITH SIMULATION |
ICAS 2008-10.10.3 (AIAA 2008-8937) |
Bhatti, J. |
AN EXPERIMENTAL AND COMPUTATIONAL COMPARISON OF THE LOW SPEED AERODYNAMICS OF SQUARE AND CIRCULAR SECTIONED BODIES |
ICAS2008-3.5 ST: |
Bil, C. |
AN ADAPTABLE METHODOLOGY FOR AUTOMATION APPLICATION DEVELOPMENT |
ICAS 2008-6.2.3 |
Bil, C. |
APPLICATION OF SHAPE OPTIMISATION TO AIRCRAFT WING STRUCTURES |
ICAS 2008-7.8.3 |
Bil, C. |
BWB MILITARY CARGO TRANSPORT FUSELAGE DESIGN AND ANALYSIS |
ICAS 2008-7.9.3 |
Bil, C. |
GENETIC FUZZY CONTROL FOR AUTONOMOUS DUCTED-FAN VTOL UAV |
ICAS 2008-5.9.3 |
Bil, C. |
KNOWLEDGE MANAGEMENT FOR THROUGH LIFE SUPPORT |
ICAS 2008-6.11.3 |
Biltgen, P. T. |
PARAMETRIC SYSTEM EFFECTIVENESS ANALYSIS USING ARTIFICIAL NEURAL NETWORKS FOR BATTLE MANAGEMENT |
ICAS 2008-1.3.3 |
Biltgen, P. T. |
UNCERTAINTY QUANTIFICATION FOR CAPABILITY-BASED SYSTEMS-OF-SYSTEMS DESIGN |
ICAS 2008-1.8.3 |
Birindelli, M. |
ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT |
ICAS2008-6.6 ST: |
Bisagni, C. |
INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS |
ICAS 2008-7.2.1 |
Bisagni, C. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
Blake, W. |
SUPERSONIC AIRCRAFT FORMATION FLYING TO INCREASE FLIGHT EFFICIENCY |
ICAS 2008-1.10.2 |
Böck, P. |
IMPACT OF ESTOL CAPABILITY ON RUNWAY CAPACITY - AN ANALYTICAL APPROACH |
ICAS 2008-11.9.4 (AIAA 2008-8933) |
Bock, S. |
"ACTIVE CORE" - A KEY TECHNOLOGY FOR MORE ENVIRONMENTALLY FRIENDLY AERO ENGINES BEING INVESTIGATED UNDER THE NEWAC PROGRAM |
ICAS 2008-4.2.1 |
Boillot, A. |
FROM BEAM MODELS TO GLOBAL 3D MODELS FOR ROBUST LANDING GEAR DESIGN |
ICAS2008-7.11 ST: |
Bolczak, C. N. |
SECURE AIRSPACE: A CRITICAL COMPONENT OF NEXTGEN'S LAYERED, ADAPTIVE SECURITY |
ICAS 2008-11.5.2 (AIAA 2008-8893) |
Bombardi, T. |
3D OBSTACLE AVOIDANCE STRATEGIES FOR UAS (UNINHABITED AERIAL SYSTEMS) MISSION PLANNING AND RE-PLANNING |
ICAS 2008-5.6.1 (AIAA 2008-8962) |
Bonazountas, M. |
92 LANDING-AVIONIC SYSTEM FOR SMALL-MEDIUM AIRCRAFT FOR AUTOMATED LANDING ON SMALL-MEDIUM AND/OR POORLY EQUIPPED AIRPORTS |
ICAS2008-P6.8 |
Bone, R. |
SAY WHO? PILOTED SIMULATION STUDY OF COMMUNICATIONS CENTERED AROUND A COCKPIT TRAFFIC DISPLAY |
ICAS 2008-10.5.1 (AIAA 2008-8895) |
Bonn, J. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
Bosbach, J. |
SCALING OF MIXED CONVECTION IN AIRCRAFT CABINS |
ICAS 2008-6.3.3 |
Botin, A. V. |
NUMERICAL AND EXPERIMENTAL STUDIES OF SHOCK INTERFERENCE IN HYPERSONIC FLOWS NEAR A CYLINDER |
ICAS2008-P2.3 |
Bourdiaudhy, K. |
A FLIGHT THRUST DECK FOR THE F100 TURBOFAN OF THE F16 AIRCRAFT |
ICAS 2008-4.5.1 |
Bouwmeester, J. G. H. |
CARBON/DYNEEMA INTRALAMINAR HYBRIDS: NEW STRATEGY TO INCREASE IMPACT RESISTANCE OR DECREASE MASS OF CARBON FIBER COMPOSITES |
ICAS 2008-7.3.4 |
Bower, G. C. |
MULTI-OBJECTIVE AIRCRAFT OPTIMIZATION FOR MINIMUM COST AND EMISSIONS OVER SPECIFIC ROUTE NETWORKS |
ICAS 2008-10.6.3 (AIAA 2008-8905) |
Brandin, J. |
A STUDY OF AN USER AND ENVIRONMENTAL FRIENDLY STORED ENERGY BASED EPU/APU-SYSTEM FOR MILITARY AEROSPACE APPLICATIONS |
ICAS 2008-6.4.5 |
Brandt, S. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
Braun, M. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
Breeman, J. |
A SIMULATION BENCHMARK FOR AIRCRAFT SURVIVABILITY ASSESSMENT |
ICAS 2008-9.3.2 |
Breitsamter, C. |
AERODYNAMIC INVESTIGATIONS ON A GENERIC FAN-IN-WING CONFIGURATION |
ICAS 2008-3.5.1 |
Breitsamter, C. |
FIN BUFFET CHARACTERISTICS OF ADVANCED TRAINER AIRCRAFT |
ICAS 2008-3.4.1 |
Brezillon, J. |
NUMERICAL AERODYNAMIC OPTIMISATIONS OF 3D HIGH-LIFT CONFIGURATIONS |
ICAS 2008-2.2.3 |
Brinton, C. |
IMPLICATION OF VARIABILITY IN AIRPORT SURFACE OPERATIONS ON 4-D TRAJECTORY PLANNING |
ICAS 2008-11.11.3 (AIAA 2008-8960) |
Brinton, C. |
MICROSCOPIC ANALYSIS OF AIRPORT SURFACE SEQUENCING |
ICAS2008-11.11 ST (AIAA 2008-8961) |
Broichhausen, K. |
A NEW APPROACH FOR CO2 REDUCTION APPLYING STATE-OF-THE-ART ENGINE AND AIRFRAME TECHNOLOGY |
ICAS2008-4.2 ST (AIAA 2008-8974) |
Broichhausen, K. |
POTENTIALS OF LIGHTER-THAN-AIR TECHNOLOGY IN FUTURE MARKETS – AN EVALUATION |
ICAS2008-P1.7 |
Broichhausen, K. |
PROMISING FUTURE AIRCRAFT CONCEPT – ESTOL |
ICAS2008-P1.8 |
Broncheau, J. W. |
SIMULATION OF A NON-AXISYMMETRIC UNDERSEA VEHICLE USING A RECURSIVE NEURAL NETWORK |
ICAS 2008-5.8.2 |
Brown, A. P. |
COMPUTATIONAL FLUID DYNAMICS AND EXPERIMENTAL INVESTIGATION OF AIRPLANE STALL DYNAMICS WITH WING CONTAMINATION |
ICAS 2008-3.5.2 |
Brown, N. |
GOING GREEN – MITIGATING AVIATION’S NEW ENVIRONMENTAL DRIVERS |
ICAS 2008-4.7.2 |
Brown, N. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
Brunet, M. |
A NOVEL APPROACH TO AIR TRANSPORT SYSTEM ENVIRONMENTAL IMPACT EVALUATION THROUGH PHYSICAL MODELLING AND SIMULATION |
ICAS2008-8.3 ST: |
Bublitsky, B. |
INNOVATIVE APPROACH FOR FUTURE AIRCRAFT DEVELOPMENT AT IAI |
ICAS 2008-1.6.1 |
Bucher, B. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
Bueno, J. |
SAFE AUTOMATIC FLIGHT BACK AND LANDING OF AIRCRAFT (SOFIA) |
ICAS2008-9.7 ST: |
Buoni, G. P. |
LARGE UAS OPERATIONS IN THE NAS - THE NASA 2007 WESTERN STATES FIRE MISSIONS |
ICAS 2008-8.1.3 (AIAA 2008-8967) |
Buonomo, B. |
VORTEX BLOB METHOD AS VISUALIZATION TOOL FOR MULTI-ELEMENT AIRFOIL FLOWS OPTIMIZATION |
ICAS 2008-3.9.2 |
Burke, R. |
AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH |
ICAS 2008-10.3.1 (AIAA 2008-8861) |
Burke, R. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
Burleson, C. |
GOING GREEN – MITIGATING AVIATION’S NEW ENVIRONMENTAL DRIVERS |
ICAS 2008-4.7.2 |
Bushnell, L. |
SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-9.1.3 |
Bussink, F. J. L. |
A PERFORMANCE ASSESSMENT OF A TACTICAL AIRBORNE SEPARATION ASSISTANCE SYSTEM USING REALISTIC, COMPLEX TRAFFIC FLOWS |
ICAS 2008-11.4.4 (AIAA 2008-8884) |
Bussink, F. J. L. |
OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM |
ICAS 2008-11.6.1 (AIAA 2008-8898) |
Bussink, F. J. L. |
PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY |
ICAS 2008-10.5.2 (AIAA 2008-8896) |
Butler, J. D. |
A STUDY OF SHEAR LAYER SUB-STRUCTURES IN LEADING EDGE VORTICES USING LASER DOPPLER VELOCIMETRY |
ICAS 2008-2.1.3 |
Butterfield, J. |
AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH |
ICAS 2008-10.3.1 (AIAA 2008-8861) |
Butterfield, J. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
Byun, Y. -H. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
Caixeta Jr., P. R. |
AERO-STRUCTURAL MDO OF A SPAR-TANK-TYPE WING FOR AIRCRAFT CONCEPTUAL DESIGN |
ICAS2008-1.1 ST: |
Calabrò, A. |
AN ORIGINAL SYSTEM TO MEASURE ADAPTIVE STRUCTURE PARAMETERS USING FIBER OPTIC |
ICAS2008-7.4 ST: |
Callantine, T. |
CONTROLLER SUPPORT FOR MANAGING HIGH-EFFICIENCY ARRIVALS IN DENSE TRAFFIC ENVIRONMENTS |
ICAS 2008-11.10.4 (AIAA 2008-8943) |
Camilo, E. |
DYNAMIC ANALYSIS OF AEROELASTIC RESPONSE FOR TRANSONIC FLOW WITH NONLINEAR STRUCTURAL MODEL |
ICAS 2008-9.6.4 |
Campos, L. M. B. C. |
391 EFFECT OF ATMOSPHERIC PROPAGATION ON AIRCRAFT NOISE |
ICAS2008-P10.1 |
Campos, L. M. B. C. |
ON THE EFFECTS ON NOISE OF GROUND REFLECTION AND ATMOSPHERIC ATTENUATION ON THE NOISE OF HELICOPTERS |
ICAS 2008-3.9.4 |
Campos, L. M. B. C. |
ON THE MINIMIZATION OF CRUISE DRAG DUE TO PITCH TRIM FOR A FLYING-WING CONFIGURATION |
ICAS 2008-5.3.3 |
Campos, L. M. B. C. |
ON THE PROBABILITY OF COLLISION FOR CLIMBING AND DESCENDING TRAJECTORIES RELEVANT TO AIR TRAFFIC MANAGEMENT |
ICAS2008-9.3 ST: |
Campos, N. V. |
PRELIMINARY ANALYSIS OF STRATEGIES AND CHALLENGES TO ENCOURAGE DATA LINK ADOPTION OVER THE NORTH ATLANTIC AIRSPACE |
ICAS 2008-8.8.3 (AIAA 2008-8953) |
Canders, R. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
Cannata, M. |
TRANSVERSAL INJECTED SYNTHETIC JETS FOR WALL TURBULENCE CONTROL |
ICAS 2008-3.10.3 |
Capello, E. |
TRAJECTORY OPTIMISATION FOR AUTONOMOUS VEHICLES: A MINIUAV APPLICATION |
ICAS 2008-5.6.3 |
Capron, W. R. |
SIMULATION RESULTS FOR AIRBORNE PRECISION SPACING ALONG CONTINUOUS DESCENT ARRIVALS |
ICAS 2008-11.9.2 (AIAA 2008-8931) |
Carbaugh, D. |
THE SAFETY GAINED BY EQUIPMENT AND PROCEDURES USED TO PERFORM CONSTANT ANGLE APPROACHES |
ICAS 2008-9.7.3 |
Carl, U. |
EVAPORATING COOLANT FOR ON-BOARD COOLING SYSTEMS WITH DIRECT CONDENSATION THROUGH AMBIENT AIR |
ICAS 2008-6.6.3 |
Carl, U. |
MULTIVARIABLE CONTROLLER DESIGN FOR A TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WITH TWO PRIMARY LOAD PATHS |
ICAS 2008-6.4.2 |
Carl, U. B. |
MONITORING OF OSCILLATORY FAILURE CASES FOR THE REDUCTION OF STRUCTURAL LOADS IN AN AEROELASTIC AIRCRAFT |
ICAS 2008-7.7.2 |
Carlomagno, G. M. |
EXPERIMENTAL ANALYSIS OF THE FLOW FIELD IN A ROTATING 'U' CHANNEL |
ICAS 2008-4.6.3 |
Carpenter, A. L. |
FLIGHT EXPERIMENTS ON SWEPT WING TRANSITION USING DISTRIBUTED ROUGHNESS |
ICAS 2008-2.7.5 |
Cassano, C. L. |
APPLICATION OF THE INTEGRATED PRODUCT TEAM (IPT) CONCEPT TO THE RE-ENGINE OF A VERY LIGHT JET (VLJ) |
ICAS 2008-6.7.5 |
Castelletti, L. M. L. |
SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT |
ICAS 2008-7.9.2 |
Castelletti, L.-M. L. |
BIRDSTRIKE ONTO STRUCTURES IN ROTATIONAL MOTION |
ICAS 2008-9.4.4 |
Castelli, L. |
CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE |
ICAS 2008-8.2.1 |
Catalano, F. M. |
AERO-STRUCTURAL MDO OF A SPAR-TANK-TYPE WING FOR AIRCRAFT CONCEPTUAL DESIGN |
ICAS2008-1.1 ST: |
Catalano, F. M. |
PASSIVE, ACTIVE AND ADAPTIVE SYSTEMS FOR WING VORTEX DRAG REDUCTION |
ICAS2008-2.7 ST: |
Cavagna, L. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
Cavagna, L. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
Cavagna, L. |
DEVELOPMENT AND VALIDATION OF AN INVESTIGATION TOOL FOR NONLINEAR AEROELASTIC ANALYSIS |
ICAS 2008-9.6.3 |
Cecrdle, J. |
EXPLOITATION OF OPTIMIZATION SOLUTION FOR DETERMINATION OF WHIRL FLUTTER STABILITY BOUNDARIES |
ICAS2008-P3.2 |
Cenko, A. |
STORE SEPARATION TRAJECTORY SIMULATION FOR THE HIGH SPEED ANTI-RADIATION DEMONSTRATOR (HSAD) FROM THE F-4 AIRCRAFT |
ICAS 2008-2.9.3 |
Cenko, A. |
TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT |
ICAS 2008-2.9.2 |
Cerón-Muñoz, H. D. |
PASSIVE, ACTIVE AND ADAPTIVE SYSTEMS FOR WING VORTEX DRAG REDUCTION |
ICAS2008-2.7 ST: |
Chai, J. Z. |
A FAST GRID DEFORMATION ALGORITHM AND IT’S APPLICATION |
ICAS2008-P2.4 |
Chamberlain, J. P. |
PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY |
ICAS 2008-10.5.2 (AIAA 2008-8896) |
Chambliss, A. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
Chang, J. -W. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
Charrier, J. -J. |
PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES |
ICAS2008-6.6 ST (AIAA 2008-8973) |
Charrier, J.-J. |
A VISION OF MORE ELECTRICAL AIRCRAFT AND CURRENT DEVELOPMENTS |
ICAS 2008-6.5.1 INVITED |
Chartrand, R. |
PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY |
ICAS 2008-10.5.2 (AIAA 2008-8896) |
Chartrand, R. C. |
OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM |
ICAS 2008-11.6.1 (AIAA 2008-8898) |
Chate, A. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
Chatterjee, T. |
LASER PROPELLED HYPERSONIC AIR-VEHICLE |
ICAS2008-4.3 ST: |
Chen, B. |
AN APPROXIMATION METHOD FOR THE NUMERICAL SIMULATION ON UNSTEADY FLOWS AROUND SMALL-DISPLACEMENT MOVING OBJECTS |
ICAS2008-3.9 ST: |
Chen, C. |
THE APPLICATION OF AIRBORNE VIDEO TECHNOLOGIES DURING AERIAL REFUELING TEST |
ICAS2008-P5.2 |
Chen, N. Y. |
ESTIMATION OF AIR TRAFFIC DELAY USING THREE DIMENSIONAL WEATHER INFORMATION |
ICAS 2008-10.7.3 (AIAA 2008-8916) |
Chen, Z. |
EFFECTS OF SUSPENSION WEIGHT ON FIGHTER FATIGUE DAMAGE |
ICAS 2008-7.4.5 |
Cheng, H. |
TEST DATA MANAGEMENT FOR AIRCRAFT HYDRAULIC SYSTEM TESTING |
ICAS2008-P6.3 |
Cheng, V. H. L. |
MODEL-BASED AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.1 (AIAA 2008-8907) |
Cheng, V. H. L. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
Cheng, W. |
ADVANCED MANUFACTURING GRID SUPPORTING AVIATION INDUSTRY EXTENSIVE COLLABORATIVE DESIGN AND SIMULATION |
ICAS2008-6.10 ST: |
Cheng, W. |
RESEARCH ON FAILURE CRITERION FOR COMPOSITE MATERIALS IN OPTIMIZATION |
ICAS 2008-7.1.2 |
Cherevko, A. |
MODERN MATHEMATICAL METHODS IN AERONAUTICAL SCIENCES |
ICAS2008-2.3 ST: |
Chiesa, S. |
ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT |
ICAS2008-6.6 ST: |
Chishty, W. A. |
DEVELOPMENT OF AN INDUSTRIAL SCALE COMBUSTION TEST AND RESEARCH FACILITY FOR ALTERNATIVE FUELS AND FUEL FLEXIBILITY DEMONSTRATION |
ICAS 2008-4.3.1 |
Cho, G. -H. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
Cho, J. |
UNSTEADY AERODYNAMIC ANALYSIS OF HELICOPTER ROTOR BY USING THE TIME-DOMAIN PANEL METHOD |
ICAS2008-2.10 ST: |
Cho, L. |
UNSTEADY AERODYNAMIC ANALYSIS OF HELICOPTER ROTOR BY USING THE TIME-DOMAIN PANEL METHOD |
ICAS2008-2.10 ST: |
Cho, S. H. |
BWB MILITARY CARGO TRANSPORT FUSELAGE DESIGN AND ANALYSIS |
ICAS 2008-7.9.3 |
Chrishti, M. |
INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS |
ICAS 2008-7.2.1 |
Chu, Y. -C. |
AUTOMATED CONFLICT RESOLUTION - A SIMULATION-BASED SENSITIVITY STUDY OF AIRSPACE AND DEMAND |
ICAS 2008-8.9.1 |
Chung, S. |
NATSIM: A SYSTEMS DYNAMICS MODEL OF NORTH ATLANTIC AIR TRAFFIC |
ICAS 2008-9.11.3 (AIAA 2008-8912) |
Chupakhin, A. |
MODERN MATHEMATICAL METHODS IN AERONAUTICAL SCIENCES |
ICAS2008-2.3 ST: |
Cisowski, J. |
MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION |
ICAS 2008-1.5.2 |
Clare, J. C. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
Clarke, A. |
DESIGN AND DEVELOPMENT OF THE ECLIPSE AND DEMON DEMONSTRATOR UAVS |
ICAS 2008-1.4.2 |
Claus, R. W. |
COUPLED HIGH-FIDELITY ENGINE SYSTEM SIMULATION |
ICAS 2008-8.10.3 INVITED |
Clay, S. |
FLIGHT VEHICLE COMPOSITE STRUCTURES |
ICAS 2008-7.9.1 (AIAA 2008-8976 ) |
Coatanéa, M. |
PRELIMINARY DESIGN OF A JOINED WING HALE UAV |
ICAS 2008-1.4.3 |
Coimbra, R. F. |
PASSIVE, ACTIVE AND ADAPTIVE SYSTEMS FOR WING VORTEX DRAG REDUCTION |
ICAS2008-2.7 ST: |
Coiro, D. P. |
SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION |
ICAS 2008-2.7.3 |
Collisson, C. |
RE-INVENTING THE LEGEND: THE DEVELOPMENT OF THE 747-8 |
ICAS 2008-1.7.3 |
Cologan, C. |
AERODYNAMIC INVESTIGATIONS ON A GENERIC FAN-IN-WING CONFIGURATION |
ICAS 2008-3.5.1 |
Comell, B. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
Consiglio, M. |
IMPACT OF PREDICTION UNCERTAINTY ON THE SAFETY PERFORMANCE OF AIRBORNE SEPARATION |
ICAS 2008-11.4.2 (AIAA 2008-8882) |
Conway, S. R. |
TOWARDS 4D TRAJECTORY MANAGEMENT: CONTAINMENT AND THE USE OF RNP IN CONSTRAINED TERMINAL AIRSPACE |
ICAS2008-8.11 ST: |
Cook, L. S. |
IMPROVED PREDICTION OF GATE DEPARTURE TIMES USING PRE-DEPARTURE EVENTS |
ICAS 2008-11.8.1 (AIAA 2008-8919) |
Cordisco, P. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
Corke, T. C. |
FOREBODY VORTEX CONTROL ON HIGH PERFORMANCE AIRCRAFT USING PWM-CONTROLLED PLASMA ACTUATORS |
ICAS 2008-3.3.4 |
Corpino, S. |
ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT |
ICAS2008-6.6 ST: |
Crescenzio, F.De |
DESIGN AND EVALUATION OF A 4D INTERFACE FOR ATC |
ICAS 2008-9.10.3 |
Crook, I. |
MULTI-OBJECTIVE OPTIMIZATION OF USER PREFERRED 4D TRAJECTORIES IN THE NAS |
ICAS 2008-11.6.2 (AIAA 2008-8899) |
Crossley, W. |
COMBINATORIAL OPTIMIZATION TO INCLUDE GREENER TECHNOLOGIES IN A SHORT-TO-MEDIUM RANGE COMMERCIAL AIRCRAFT |
ICAS 2008-4.10.2 (AIAA 2008-8963) |
Crossley, W. A. |
BASE OF OPERATIONS CONCEPT FOR ON-DEMAND OPERATIONS |
ICAS 2008-8.6.4 (AIAA 2008-8977 ) |
Crossley, W. A. |
CONCURRENT AIRCRAFT DESIGN AND RESOURCE ALLOCATION UNDER UNCERTAINTY FOR ON-DEMAND AIR TRANSPORTATION |
ICAS 2008-10.6.1 (AIAA 2008-8903) |
Cui, D. |
ADVANCED MANUFACTURING GRID SUPPORTING AVIATION INDUSTRY EXTENSIVE COLLABORATIVE DESIGN AND SIMULATION |
ICAS2008-6.10 ST: |
Cui, D. |
RESEARCH ON FAILURE CRITERION FOR COMPOSITE MATERIALS IN OPTIMIZATION |
ICAS 2008-7.1.2 |
Curran, R. |
AEROSPACE PRODUCT COST MANAGEMENT AT THE EARLY CONCEPT OPERATIONS PHASE |
ICAS 2008-10.6.2 (AIAA 2008-8904) |
Curran, R. |
AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH |
ICAS 2008-10.3.1 (AIAA 2008-8861) |
Curran, R. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
Curran, R. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
Da Ronch, A. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
da Silva, R. G. |
AN AERODYNAMIC OPTIMIZATION FRAMEWORK BASED ON GENETIC ALGORITHMS |
ICAS 2008-2.3.4 |
Dao, A. Q. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
Dartois, S. |
A MULTI-SCALE “MORPHOLOGICAL APPROACH” FOR MODELING THE NON LINEAR BEHAVIOR OF PROPELLANT-LIKE MATERIALS |
ICAS 2008-7.1.3 |
De Crescenzio, F. |
3D OBSTACLE AVOIDANCE STRATEGIES FOR UAS (UNINHABITED AERIAL SYSTEMS) MISSION PLANNING AND RE-PLANNING |
ICAS 2008-5.6.1 (AIAA 2008-8962) |
De Crescenzio, F. |
DESIGN AND DEVELOPMENT OF AN ATC DISTRIBUTED TRAINING SYSTEM |
ICAS2008-P8.2 (AIAA 2008-8873) |
de Gelder, N. |
ENABLING TECHNOLOGY EVALUATION FOR EFFICIENT CONTINUOUS DESCENT APPROACHES |
ICAS 2008-8.9.2 |
de Jong, H. H. |
A PROGNOSTIC METHOD TO IDENTIFY HAZARDS FOR FUTURE AVIATION CONCEPTS |
ICAS 2008-9.3.1 |
de Jong, J. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
de Kat, R. |
VORTEX WAKE INVESTIGATION BEHIND A WING-FLAP MODEL WITH JET SIMULATION |
ICAS 2008-3.9.1 |
de Muynck, R. J. |
ENABLING TECHNOLOGY EVALUATION FOR EFFICIENT CONTINUOUS DESCENT APPROACHES |
ICAS 2008-8.9.2 |
de Oliveira Neto, J. A. |
APPLICATION OF A NAVIER-STOKES CODE TO THE SIMULATIONS OF HIGH-LIFT DEVICES USING UNSTRUCTURED GRIDS |
ICAS 2008-2.2.4 |
De Tenorio, C. |
FUNCTION BASED ARCHITECTURE DESIGN SPACE DEFINITION AND EXPLORATION |
ICAS 2008-1.9.3 (AIAA 2008-8928) |
de Tenorio, C. |
METHODOLOGY FOR AIRCRAFT SYSTEM ARCHITECTURE SIZING |
ICAS 2008-6.2.2 |
De Visscher, I. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
de Ward, A. |
DESIGN OF A LEAN MRO BUSINESS PROCESS FOR EPCOR |
ICAS 2008-10.3.4 (AIAA 2008-8864) |
de Witte, T. D. |
A PRACTICAL APPROACH TO MULTI-OBJECTIVE CAPACITY ANALYSIS OF AN ENVIRONMENT-AWARE AIRPORT |
ICAS 2008-8.5.1 |
DeArmon, J. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
Decours, J. |
AERODYNAMIC AND AERO-ACOUSTIC DESIGN OF MODERN TILT-ROTORS: THE ONERA EXPERIENCE |
ICAS 2008-1.7.4 |
DeGarmo, M. |
NEXTGEN AND SESAR: OPPORTUNITIES FOR UAS INTEGRATION |
ICAS 2008-10.8.2 (AIAA 2008-8925) |
Degenhardt, R. |
COLLAPSE BEHAVIOR OF THIN-WALLED CFRP STRUCTURES DUE TO MATERIAL AND GEOMETRIC NONLINEARITIES–EXPERIMENTS AND SIMULATION |
ICAS 2008-7.11.3 |
Degenhardt, R. |
THE DESIGN OF POSTBUCKLING COMPOSITE AEROSPACE STRUCTURES ACCOUNTING FOR DAMAGE INITIATION AND GROWTH |
ICAS 2008-7.3.2 |
Delannoy, A. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
DeLaurentis, D. A. |
A NEW SYSTEMS ANALYSIS: PERSPECTIVES ON SYSTEM-OF-SYSTEMS AND REGIONAL TRANSPORTATION PROOF-OF-CONCEPT STUDY |
ICAS 2008-1.3.2 |
DeLaurentis, D. A. |
UTILIZATION OF NETWORK THEORY FOR THE ENHANCEMENT OF ATO AIR ROUTE FORECAST |
ICAS 2008-11.10.5 (AIAA 2008-8944) |
Deligiannidis, N. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
Deloach, R. |
ESTIMATION OF SUPERSONIC STAGE SEPARATION AERODYNAMICS OF WINGED-BODY LAUNCH VEHICLES USING RESPONSE SURFACE METHODS |
ICAS 2008-3.1.1 |
Denegri Jr., C. M. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
Deng, Y. C. |
OPTIMIZATION DESIGN ON PLATE-RIB STRUCTURE FOR CERTAIN KINDS OF AIRCRAFT |
ICAS 2008-9.5.3 |
Deremaux, Y. |
DESIGN OF A SMALL SUPERSONIC TRANSPORT AIRCRAFT WITH HIGH ENVIRONMENTAL CONSTRAINTS |
ICAS 2008-1.10.1 INVITED |
Deremeaux, Y. |
UNCERTAINTIES AT THE CONCEPTUAL STAGE: MULTILEVEL MULTIDISCIPLINARY DESIGN AND OPTIMIZATION APPROACH |
ICAS 2008-1.1.2 |
Deslandes, R. |
IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT |
ICAS 2008-2.6.2 |
d'Espiney, P. |
WHITE LIGHT SKIN-FRICTION AND GAS DENSITY MEASUREMENTS AROUND A SUPERSONIC FOREBODY |
ICAS 2008-3.8.2 |
Desse, J. M. |
WHITE LIGHT SKIN-FRICTION AND GAS DENSITY MEASUREMENTS AROUND A SUPERSONIC FOREBODY |
ICAS 2008-3.8.2 |
Devenny, C. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
Di Cicca, G. M. |
LARGE-SCALE MANIPULATION OF A TURBULENT BOUNDARY LAYER BY MEANS OF A 2D SYNTHETIC JET |
ICAS2008-P2.8 |
Di Landro, L. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
Díaz, J. |
THERMAL DESIGN UNDER UNCERTAINTIES OF AIRCRAFT STRUCTURES |
ICAS 2008-7.2.3 |
Dignum, V. |
AN ONTOLOGY FOR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-9.11.1 (AIAA 2008-8946) |
Dillenius, M. |
IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT |
ICAS 2008-2.6.2 |
Dinh, Q. V. |
UNCERTAINTIES AT THE CONCEPTUAL STAGE: MULTILEVEL MULTIDISCIPLINARY DESIGN AND OPTIMIZATION APPROACH |
ICAS 2008-1.1.2 |
Dircken, F. |
CONTROLLABILITY OF BLENDED WING BODY AIRCRAFT |
ICAS 2008-5.4.3 |
Djojodihardjo, H. |
UNIFIED BE-FE AERODYNAMIC-ACOUSTIC-STRUCTURE COUPLING SCHEME FOR ACOUSTIC EFFECTS ON AEROELASTIC STRUCTURES |
ICAS 2008-7.7.3 |
Doble, N. A. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
Dodbelle, S. |
STORE SEPARATION TRAJECTORY SIMULATION FOR THE HIGH SPEED ANTI-RADIATION DEMONSTRATOR (HSAD) FROM THE F-4 AIRCRAFT |
ICAS 2008-2.9.3 |
Doherty, J. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
Doll, C. |
MODELLING OF THE 3-DOF NONLINEAR AIRCRAFT BEHAVIOUR VIA SMALL STANDARD FORMS |
ICAS2008-P5.5 |
Domino, D. A. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
Donnerhack, S. |
A NEW APPROACH FOR CO2 REDUCTION APPLYING STATE-OF-THE-ART ENGINE AND AIRFRAME TECHNOLOGY |
ICAS2008-4.2 ST (AIAA 2008-8974) |
Dorgan, A. |
A HYBRID, DYNAMIC LARGE EDDY SIMULATION METHOD |
ICAS 2008-2.1.1 |
Dowell, E. H. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
Dr?g??anu, C. |
AUTOMATIC FLIGHT CONTROL USING SAMPLED-DATA MIXED H_2/H_INFINITY OPTIMISATION |
ICAS 2008-5.2.1 |
Dragon, A. |
A MULTI-SCALE “MORPHOLOGICAL APPROACH” FOR MODELING THE NON LINEAR BEHAVIOR OF PROPELLANT-LIKE MATERIALS |
ICAS 2008-7.1.3 |
Dray, L. |
MODELLING AIRLINE ROUTING AND SCHEDULING UNDER AIRPORT CAPACITY CONSTRAINTS |
ICAS 2008-11.1.2 (AIAA 2008-8855) |
Dray, L. M. |
NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY |
ICAS 2008-10.4.4 (AIAA 2008-8890) |
Dron, S. |
TOWARD ACARE 2020: INNOVATIVE ENGINE ARCHITECTURES TO ACHIEVE THE ENVIRONMENTAL GOALS? |
ICAS 2008-4.2.2 |
Duan, X. |
TERRAIN FOLLOWING FLIGHT REAL-TIME HIL SIMULATION PLATFORM RESEARCH |
ICAS2008-P5.6 |
Duffy, M. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
Duong, V. |
ANALYSIS OF GAPS BETWEEN THE PREDICTIVE AND THE ADAPTIVE COMPONENT IN ATM |
ICAS 2008-11.10.2 (AIAA 2008-8941) |
Duong, V. |
HARMONIZING AUTOMATION, PILOT AND AIR TRAFFIC CONTROLLER IN THE FUTURE AIR TRAFFIC MANAGEMENT |
ICAS 2008-8.2.4 |
D'Urso, S. D. |
FLIGHT DYNAMICS OF THE FLYING WING |
ICAS 2008-5.8.3 |
Dwight, R. P. |
NUMERICAL AERODYNAMIC OPTIMISATIONS OF 3D HIGH-LIFT CONFIGURATIONS |
ICAS 2008-2.2.3 |
Early, J. M. |
EXCRESCENCES EFFECTS IN AERODYNAMICS |
ICAS2008-3.8 ST: |
Edinger, C. |
INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS |
ICAS 2008-8.4.5 |
Edinger, C. |
PERFORMANCE-BASED TMA HANDLING FOR MIXED TRAFFIC USING A GROUND BASED 4D-GUIDANCE FOR UNEQUIPPED AIRCRAFT |
ICAS 2008-10.8.3 |
Egami, Y. |
DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS |
ICAS 2008-3.2.1 |
Egbert, N. |
DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS |
ICAS 2008-6.7.4 |
Eglitis, E. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
Eijgelshoven, T. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
Elangovan, R. |
MODELING OF ACOUSTICALLY TREATED NACELLE LIP TRANSPIRATION FLOW ANTI-ICING SYSTEM |
ICAS 2008-6.4.3 |
Elfstrom, G. M. |
DESIGN AND OPERATION OF THE ADD ENVIRONMENTAL TEST FACILITY |
ICAS2008-P6.6 |
Elliff, T. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Elmer, K. R. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
Empringham, L. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
Engelland, S. A. |
MICROSCOPIC ANALYSIS OF AIRPORT SURFACE SEQUENCING |
ICAS2008-11.11 ST (AIAA 2008-8961) |
Engert, M. |
ACTIVE CANCELLATION OF TOLLMIEN-SCHLICHTING INSTABILITIES UP TO M = 0.40 |
ICAS 2008-3.10.2 |
Entzinger, J. O. |
MODELING OF THE VISUAL APPROACH TO LANDING USING NEURAL NETWORKS AND FUZZY SUPERVISORY CONTROL |
ICAS 2008-5.1.3 |
Epstein, B. |
EFFICIENT APPROACH FOR MULTIPOINT AERODYNAMIC WING DESIGN OF BUSINESS JET AIRCRAFT |
ICAS 2008-2.11.1 |
Epstein, B. |
HYBRIDIZATION OF HETEROGENEOUS 3D CFD DISCRETIZATIONS VIA DIRECT FLUX OPTIMIZATION |
ICAS2008-2.3 ST: |
Erdem, E. |
THE INVESTIGATION OF DEPENDENCE OF LOW FREQUENCY MOTION ON UPSTREAM FLOW CONDITIONS IN HYPERSONIC FLOWS |
ICAS2008-3.7 ST: |
Erickson, G. |
ESTIMATION OF SUPERSONIC STAGE SEPARATION AERODYNAMICS OF WINGED-BODY LAUNCH VEHICLES USING RESPONSE SURFACE METHODS |
ICAS 2008-3.1.1 |
Eriksen, P. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
Erzberger, H. |
ALGORITHM AND OPERATIONAL CONCEPT FOR RESOLVING SHORT-RANGE CONFLICTS |
ICAS 2008-8.7.5 |
Erzberger, H. |
AUTOMATED CONFLICT RESOLUTION - A SIMULATION-BASED SENSITIVITY STUDY OF AIRSPACE AND DEMAND |
ICAS 2008-8.9.1 |
Estkowski, R. |
REAL-TIME SIMULATION OF A DISTRIBUTED CONFLICT RESOLUTION ALGORITHM |
ICAS 2008-8.7.3 |
Evans, A. |
NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY |
ICAS 2008-10.4.4 (AIAA 2008-8890) |
Evans, A. D. |
MODELLING AIRLINE ROUTING AND SCHEDULING UNDER AIRPORT CAPACITY CONSTRAINTS |
ICAS 2008-11.1.2 (AIAA 2008-8855) |
Everdij, M. H. C. |
A PROGNOSTIC METHOD TO IDENTIFY HAZARDS FOR FUTURE AVIATION CONCEPTS |
ICAS 2008-9.3.1 |
Eyers, C. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Fabiani, P. |
PERSPECTIVES ON (MULTI-) UAV OPERATIONS: AUTONOMY & SECURITY ISSUES |
ICAS 2008-6.8.3 INVITED |
Falk, R. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
Faller, W. E. |
SIMULATION OF A NON-AXISYMMETRIC UNDERSEA VEHICLE USING A RECURSIVE NEURAL NETWORK |
ICAS 2008-5.8.2 |
Fanget, A. |
A MULTI-SCALE “MORPHOLOGICAL APPROACH” FOR MODELING THE NON LINEAR BEHAVIOR OF PROPELLANT-LIKE MATERIALS |
ICAS 2008-7.1.3 |
Farahmand, B. |
COHESIVE DISINTEGRATION IN IMPACTED RE-ENTRY SPACE TRANSPORTATION HYBRID STRUCTURES |
ICAS 2008-7.5.1 |
Farahmand, R. |
PREDICTION OF DELAMINATION IN ADVANCED AEROSPACE COMPOSITE STRUCTURES USING MICRO/MACRO MECHANICS CONSTITUTIVE METHODS |
ICAS 2008-7.5.3 |
Farley, T. |
AUTOMATED CONFLICT RESOLUTION - A SIMULATION-BASED SENSITIVITY STUDY OF AIRSPACE AND DEMAND |
ICAS 2008-8.9.1 |
Fasano, G. |
DEVELOPMENT AND TEST OF AN INTEGRATED SENSOR SYSTEM FOR AUTONOMOUS COLLISION AVOIDANCE |
ICAS2008-P6.12 |
Fasel, H. F. |
INVESTIGATION OF SEPARATION CONTROL FOR LOW-PRESSURE TURBINES USING CFD |
ICAS 2008-4.4.2 |
Fazli, N. |
EFFECTS OF HIERARCHY ORDER ON NATURAL FREQUENCY AND VIBRATION TRANSMISSION OF SELF-SIMILAR TRUSSES |
ICAS2008-P3.9 |
Feih, S. |
LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS |
ICAS 2008-7.2.2 |
Feldman, G. R. |
VISAGE - A NEW VISION FOR GEOSPATIAL DATA VISUALIZATION AND ANALYSIS |
ICAS2008-P8.1 (AIAA 2008-8872) |
Féru, F. |
SYSTEM INFRASTRUCTURE FOR INTEGRATED AND COLLABORATIVE PRODUCT DEVELOPMENT IN THE AERONAUTIC INDUSTRY |
ICAS 2008-6.10.2 |
Fey, U. |
DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS |
ICAS 2008-3.2.1 |
Fielding, J. P. |
DESIGN AND DEVELOPMENT OF THE ECLIPSE AND DEMON DEMONSTRATOR UAVS |
ICAS 2008-1.4.2 |
Fielding, J. P. |
NOVEL DESIGN CONCEPTS FOR AIRCRAFT WITH REDUCED NOISE AND GLOBAL WARMING CHARACTERISTICS |
ICAS 2008-4.10.4 |
Fielding, J. P. |
RECENT DEVELOPMENTS OF MSG-3 (MAINTANANCE STEERING GROUP) GUIDANCE FOR THE CONTINUED AIRWORTHINESS OF LIGHTNING/HIRF PROTECTION AND BENFITS TO NEW AIRPLANE DESIGN |
ICAS 2008-9.4.5 (AIAA 2008-8964 ) |
Filatyev, A. S. |
AEROSPACE TRAJECTORY OPTIMIZATION: NOVEL VIEW ON A ROLE OF ATMOSPHERIC FLIGHT |
ICAS 2008-5.3.1 |
Fleming, G. |
PAYLOAD FUEL ENERGY EFFICIENCY AS A METRIC FOR AVIATION ENVIRONMENTAL PERFORMANCE |
ICAS 2008-4.7.4 |
Fleming, G. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Fofonov, D. |
NUMERICAL SIMULATION OF VISCOUS FLOWS AROUND LIFTING BODIES OF COMPLICATED CONFIGURATION |
ICAS 2008-2.6.3 |
Follet, J. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
Fong, C. -C. V. |
SECURE AIRSPACE: A CRITICAL COMPONENT OF NEXTGEN'S LAYERED, ADAPTIVE SECURITY |
ICAS 2008-11.5.2 (AIAA 2008-8893) |
Fong, R. K. |
DEVELOPMENT AND APPLICATION OF AN INTEGRATED APPROACH TOWARD NASA AIRSPACE SYSTEMS RESEARCH |
ICAS 2008-10.8.1 (AIAA 2008-8924) |
Fonseca, A. |
ON THE DEVELOPMENT OF METHODS AND TECHNIQUES FOR AIRCRAFT STRUCTURAL HEALTH MONITORING |
ICAS2008-7.4 ST: |
Forster, C. |
AN INTEGRATED USER-ORIENTED WEATHER FORECAST SYSTEM FOR AIR TRAFFIC USING REAL-TIME OBSERVATIONS AND MODEL DATA |
ICAS 2008-8.6.3 |
Forster, C. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
Forster, E. |
FLIGHT VEHICLE COMPOSITE STRUCTURES |
ICAS 2008-7.9.1 (AIAA 2008-8976 ) |
Fortin, F. |
TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT |
ICAS 2008-2.9.2 |
Francesconi, E. |
SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT |
ICAS 2008-7.9.2 |
Francis, M. S. |
DESIGN OF NEXT GENERATION UNMANNED AIR SYSTEMS - ISSUES AND OPPORTUNITIES |
ICAS 2008-1.4.1 INVITED |
Friehmelt, H. |
KEY EXAMPLES AND POTENTIAL OF AVIATION YOUTH PROGRAMS IN GERMANY |
ICAS 2008-6.9.3 |
Frossard, P. L. |
SYSTEM INFRASTRUCTURE FOR INTEGRATED AND COLLABORATIVE PRODUCT DEVELOPMENT IN THE AERONAUTIC INDUSTRY |
ICAS 2008-6.10.2 |
Frota, J. |
NACRE EUROPEAN PROJECT PROGRESS SUMMARY |
ICAS 2008-1.7.2 |
Fry, D. N. |
A NEW SYSTEMS ANALYSIS: PERSPECTIVES ON SYSTEM-OF-SYSTEMS AND REGIONAL TRANSPORTATION PROOF-OF-CONCEPT STUDY |
ICAS 2008-1.3.2 |
Frydrychewicz, A. |
MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION |
ICAS 2008-1.5.2 |
Fukuda, Y. |
DESIGN OF OPERATION DATABASE FOR ATM PERFORMANCE ASSESSMENT |
ICAS 2008-8.9.4 |
Fumagalli, A. |
BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS |
ICAS 2008-9.10.4 |
Fürstenau, N. |
AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION |
ICAS 2008-8.3.1 |
Gaertner, N. |
ON-DEMAND SPECIAL USE AIRSPACE |
ICAS 2008-10.10.4 (AIAA 2008-8938) |
Gai, S. L. |
DRAG AND FLOW REGIMES ASSOCIATED WITH RECTANGULAR CAVITIES AT YAW AT LOW SPEEDS |
ICAS2008-P2.13 |
Galaktionov, A. |
NUMERICAL SIMULATION OF VISCOUS FLOWS AROUND LIFTING BODIES OF COMPLICATED CONFIGURATION |
ICAS 2008-2.6.3 |
Galbraith, R. A . McD. |
PERFORMANCE DEGRADATION OF A SIMULATED ICE CONTAMINATED AIRFOIL BY SUPER-COOLED DROPLETS |
ICAS 2008-3.7.2 |
Gallo, M. |
EXPERIMENTAL ANALYSIS OF THE FLOW FIELD IN A ROTATING 'U' CHANNEL |
ICAS 2008-4.6.3 |
Gao, C. |
TRANSONIC FLUTTER ANALYSIS OF AN AIRFOIL WITH APPROXIMATE BOUNDARY METHOD |
ICAS 2008-7.10.5 |
Gao, Z. |
THE APPLICATION OF ASEXUAL DNA ALGORITHM TO AIRFOIL DESIGN |
ICAS 2008-2.3.3 |
Gao, Z. H |
RESEARCH ON CONTROL ALLOCATION FOR AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS |
ICAS 2008-5.2.4 |
Gao, Z. H. |
RESEARCH ON FUZZY LOGIC PIO DETECTOR |
ICAS 2008-5.4.5 |
Garcia, A. N. |
SIMPLIFYING MSD MODELING BY USING CONTINUING DAMAGE ASSUMPTION AND PARAMETRIC STUDY: THE ROLE OF RIVET SQUEEZE FORCE |
ICAS 2008-9.8.1 |
Garcia, E |
FUNCTION BASED ARCHITECTURE DESIGN SPACE DEFINITION AND EXPLORATION |
ICAS 2008-1.9.3 (AIAA 2008-8928) |
Garcia, E. |
A METHODOLOGICAL APPROACH FOR AIRPORT TECHNOLOGY EVALUATION AND SELECTION |
ICAS 2008-8.3.4 (AIAA 2008-8965) |
Garcia, E. |
METHODOLOGY FOR AIRCRAFT SYSTEM ARCHITECTURE SIZING |
ICAS 2008-6.2.2 |
Garcia, E. |
PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES |
ICAS2008-6.6 ST (AIAA 2008-8973) |
Garcia-Chico, J. L. |
TASK ANALYSIS FOR FEASIBILITY ASSESSMENT OF A COLLABORATIVE TRAFFIC FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.7.3 (AIAA 2008-8909) |
Garrett, J. S. |
AVIATION TELEMEDICINE: PAST, PRESENT AND FUTURE |
ICAS 2008-9.2.2 |
Gati, B. |
PARAMETER IDENTIFICATION OF FLYING WING WITH SIGNIFICANT DEFORMATION |
ICAS 2008-5.8.1 |
Gatto, C. |
TRAJECTORY TRACKING FOR A NON - CONVENTIONAL UAV |
ICAS2008-P5.3 |
Gauci, J. |
A RAPID SCENARIO GENERATION TOOL FOR REPEATABLE SIMULATED TRAFFIC CONFLICTS IN FLIGHT SIMULATION |
ICAS 2008-5.1.1 INVITED |
Gauci, J. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
Gavel, H. |
A QUANTIFIED RELATIONSHIP MATRIX AIDED BY PROBABILISTIC DESIGN AND OPTIMIZATION |
ICAS 2008-6.2.1 |
Gavrilets, V. |
DAMAGE TOLERANT FLIGHT CONTROL SYSTEMS FOR UNMANNED AIRCRAFT |
ICAS 2008-6.8.1 INVITED |
Gawale, A. C. |
DESIGN, FABRICATION AND OPERATION OF REMOTELY CONTROLLED AIRSHIPS IN INDIA |
ICAS 2008-10.1.3 (AIAA 2008-8853) |
Gehri, A. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
Genc, M. |
AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF LOW RE NUMBER TRANSITIONAL FLOWS OVER AN AEROFOIL WITH LEADING EDGE SLAT |
ICAS2008-P2.1 (AIAA 2008-8877) |
Gerz, T. |
PERFORMANCE OF THE WAKE VORTEX PREDICTION AND MONITORING SYSTEM WSVBS AT FRANKFURT AIRPORT |
ICAS 2008-8.11.2 |
Ghavami, G. |
AN ANALYTICAL MODEL FOR PREDICTION OF THE STEADY STATE CREEP DEFORMATIONS AND STRESSES OF SHORT FIBER COMPOSITES |
ICAS 2008-9.8.3 |
Ghedaifi, W. |
A NOVEL APPROACH TO AIR TRANSPORT SYSTEM ENVIRONMENTAL IMPACT EVALUATION THROUGH PHYSICAL MODELLING AND SIMULATION |
ICAS2008-8.3 ST: |
Ghobbar, A. |
INTERMITTENT DEMAND FORECAST BY COMBINING THE FORECASTS FROM SEVERAL METHODS INTO A COMPOSITE ONE WITHIN MRO SECTOR |
ICAS 2008-10.3.3 (AIAA 2008-8863) |
Ghoreyshi, M. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
Gier, J. |
PREPARING LP TURBINE TECHNOLOGY FOR MODERN AIRCRAFT ENGINES |
ICAS 2008-4.6.1 |
Gilmour, M. |
AEROSPACE PRODUCT COST MANAGEMENT AT THE EARLY CONCEPT OPERATIONS PHASE |
ICAS 2008-10.6.2 (AIAA 2008-8904) |
Giordano, R. |
MODULATION TRANSFER FUNCTION OF STEREO PARTICLE IMAGE VELOCIMETRY TECHNIQUE |
ICAS2008-P2.6 |
Giris, S. |
DEVELOPING THE NEXT GENERATION OF GLOBAL GAS TURBINE ENGINEERS |
ICAS 2008-8.10.1 INVITED |
Godiksen III, W. H. |
TARGETING POD EFFECTS ON WEAPONS RELEASE FROM THE F-18C HORNET |
ICAS 2008-2.9.4 |
Goetzendorf-Grabowski, T. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
Golia, C. |
ANALYSIS OF THERMOCHEMICAL MODELING AND SURFACE CATALYTICITY IN SPACE VEHICLES REENTRY |
ICAS 2008-3.6.2 |
Golia, C. |
VORTEX BLOB METHOD AS VISUALIZATION TOOL FOR MULTI-ELEMENT AIRFOIL FLOWS OPTIMIZATION |
ICAS 2008-3.9.2 |
Golikov, A. A. |
AEROSPACE TRAJECTORY OPTIMIZATION: NOVEL VIEW ON A ROLE OF ATMOSPHERIC FLIGHT |
ICAS 2008-5.3.1 |
Gollnick, V. |
A HOLISTIC APPROACH TO EVALUATE THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-8.4.2 |
Gologan, C. |
CONCEPTUAL DESIGN OF A STOL REGIONAL-JET WITH HYBRID PROPULSION SYSTEM |
ICAS 2008-1.2.1 |
Gologan, C. |
IMPACT OF ESTOL CAPABILITY ON RUNWAY CAPACITY - AN ANALYTICAL APPROACH |
ICAS 2008-11.9.4 (AIAA 2008-8933) |
Gomes da Costa, T. F. G. |
INFLUENCES INVESTIGATION OF NUMERICAL PARAMETERS AND MESHING ON THE AEROELASTIC RESPONSE |
ICAS2008- P3.4 |
Gomes da Costa, T. F. G. |
NUMERICAL DEVELOPMENT OF A FLUTTER ACTIVE CONTROL SYSTEM BASED ON PRESSURE FEEDBACK. |
ICAS2008-P3.3 |
Gonzalez-Perez, H. |
CAPACITY MODELLING FOR FUTURE AERONAUTICAL SAFETY COMMUNICATIONS OVER WIDE AREAS |
ICAS 2008-8.8.2 (AIAA 2008-8952) |
Gooden, J. H. M. |
PIV FLOW MEASUREMENTS FOR A HIGH LIFT AIRFOIL WITH LEADING EDGE ICE |
ICAS 2008-3.7.4 |
Goraj, Z. |
MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION |
ICAS 2008-1.5.2 |
Gore, B. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
Gore, D. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
Gorrell, S. |
NUMERICAL INVESTIGATION OF INLET DISTORTION INDUCED SWIRL IN MULTISTAGE FANS |
ICAS 2008-4.4.3 |
Goulain, M. |
AIRBUS: TOWARDS AN ECO-EFFICIENT ENTERPRISE |
ICAS 2008-4.7.1 INVITED |
Graff, T. J. |
OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM |
ICAS 2008-11.6.1 (AIAA 2008-8898) |
Graham, M. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
Granada, S. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
Grandi, F. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Gray, L. |
SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT |
ICAS 2008-11.2.2 (AIAA 2008-8858) |
Greco Jr., P. C. |
APPLICATION OF A MODEL UPDATING METHOD TO AN AIRCRAFT LONGITUDINAL STABILITY AUGMENTATION SYSTEM |
ICAS2008-5.2 ST: |
Green, J. |
ICAS - THE FIRST 50 YEARS |
ICAS 2008-0.4 |
Greenbaum, D. |
METHODOLOGIES FOR ESTIMATING THE IMPACT OF SEVERE WEATHER ON AIRSPACE CAPACITY |
ICAS 2008-10.7.4 (AIAA 2008-8917) |
Greenberg, J. B. |
PULSATING COMBUSTION OF AN ORGANIC GEL-FUEL DROPLET AND ITS INFLUENCE ON THE THERMAL FIELD OF A SPRAY DIFFUSION FLAME |
ICAS 2008-4.1.2 |
Greenwell, D. I. |
MODELLING OF STATIC AERODYNAMICS OF HELICOPTER UNDERSLUNG LOADS |
ICAS 2008-5.11.2 |
Grendysa, W. |
MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION |
ICAS 2008-1.5.2 |
Grillo, C. |
TRAJECTORY TRACKING FOR A NON - CONVENTIONAL UAV |
ICAS2008-P5.3 |
Grimaldi, A. |
FE STUDY OF WINDSHIELD SUBJECTED TO HIGH SPEED BIRD IMPACT |
ICAS 2008-9.4.3 |
Groeneweg, J. |
PILOTED SIMULATION RESULTS OF AN ONBOARD WAKE VORTEX DETECTION, WARNING AND AVOIDANCE SYSTEM AND COCKPIT DISPLAY ASPECTS |
ICAS 2008-9.9.1 |
Gross, A. |
INVESTIGATION OF SEPARATION CONTROL FOR LOW-PRESSURE TURBINES USING CFD |
ICAS 2008-4.4.2 |
Grün, G. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
Grünewald, M. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
Guardone, A. |
COMPRESSIBLE FLUID-FLOW ALE FORMULATION ON CHANGING TOPOLOGY MESHES FOR AEROELASTIC SIMULATIONS |
ICAS2008-2.10 ST: |
Guellec, P. |
SYSTEM INFRASTRUCTURE FOR INTEGRATED AND COLLABORATIVE PRODUCT DEVELOPMENT IN THE AERONAUTIC INDUSTRY |
ICAS 2008-6.10.2 |
Guglieri, G. |
TRAJECTORY OPTIMISATION FOR AUTONOMOUS VEHICLES: A MINIUAV APPLICATION |
ICAS 2008-5.6.3 |
Guibert, S. |
CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE |
ICAS 2008-8.2.1 |
Guichard, L. |
CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE |
ICAS 2008-8.2.1 |
Guida, M. |
FE STUDY OF WINDSHIELD SUBJECTED TO HIGH SPEED BIRD IMPACT |
ICAS 2008-9.4.3 |
Guiler, R. W. |
CONTROL OF A SWEPT WING TAILLESS AIRCRAFT THROUGH WING MORPHING |
ICAS 2008-2.7.1 |
Guillaume, M. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
Guillou, Y. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
Gulding, J. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
Gunnion, A. J. |
LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS |
ICAS 2008-7.2.2 |
Guo, S. |
DEVELOPMENT OF A RUDDERLESS AEROELASTIC FIN TECHNOLOGY |
ICAS 2008-7.10.2 |
Guo, Y. |
STUDY ON THE RELATIONSHIP BETWEEN CORROSION DAMAGE AND RESIDUAL STRENGTH OF AL 7075-T6 ALLOY |
ICAS 2008-9.8.2 |
Gupta, A. |
LASER PROPELLED HYPERSONIC AIR-VEHICLE |
ICAS2008-4.3 ST: |
Gwiggner, C. |
ANALYSIS OF GAPS BETWEEN THE PREDICTIVE AND THE ADAPTIVE COMPONENT IN ATM |
ICAS 2008-11.10.2 (AIAA 2008-8941) |
György, R. |
POTENTIALS OF LIGHTER-THAN-AIR TECHNOLOGY IN FUTURE MARKETS – AN EVALUATION |
ICAS2008-P1.7 |
Hahn, K. -U. |
ALLEVIATION OF ATMOSPHERIC FLOW DISTURBANCE EFFECTS ON AIRCRAFT RESPONSE |
ICAS 2008-5.2.2 |
Haigermoser, C. |
INVESTIGATION OF THE FLOW IN A RECTANGULAR CAVITY USING TOMOGRAPHIC AND TIME-RESOLVED PIV |
ICAS 2008-3.2.2 |
Haigermoser, C. |
THE EFFECTS OF WALL ROUGHNESS ON THE TURBULENT BOUNDARY LAYER |
ICAS 2008-3.8.1 |
Hall, K. C. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
Hallberg, E. |
IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT |
ICAS 2008-2.6.2 |
Hallberg, E. N. |
STORE SEPARATION TRAJECTORY SIMULATION FOR THE HIGH SPEED ANTI-RADIATION DEMONSTRATOR (HSAD) FROM THE F-4 AIRCRAFT |
ICAS 2008-2.9.3 |
Hallberg, E. N. |
TARGETING POD EFFECTS ON WEAPONS RELEASE FROM THE F-18C HORNET |
ICAS 2008-2.9.4 |
Halle, W. |
AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION |
ICAS 2008-8.3.1 |
Hammond, D. W. |
A LAYER PAVEMENT MODEL TO SIMULATE ROUGHNESS FEATURES IN ICE ACCRETION NUMERICAL SIMULATION |
ICAS 2008-2.6.1 |
Han, C. H. |
UNSTEADY PROPULSIVE CHARACTERISTICS OF BIOFOILS MOVING IN A VERY LOW-REYNOLDS NUMBER FLOW |
ICAS 2008-3.9.3 |
Han, E.-P. |
UTILIZATION OF NETWORK THEORY FOR THE ENHANCEMENT OF ATO AIR ROUTE FORECAST |
ICAS 2008-11.10.5 (AIAA 2008-8944) |
Han, X. L. |
A FAST GRID DEFORMATION ALGORITHM AND IT’S APPLICATION |
ICAS2008-P2.4 |
Hansman, R. J. |
ANALYSIS OF INTERACTION BETWEEN AIR TRANSPORTATION AND ECONOMIC ACTIVITY |
ICAS 2008-10.4.2 (AIAA 2008-8888) |
Hansman, R. J. |
PRELIMINARY ANALYSIS OF STRATEGIES AND CHALLENGES TO ENCOURAGE DATA LINK ADOPTION OVER THE NORTH ATLANTIC AIRSPACE |
ICAS 2008-8.8.3 (AIAA 2008-8953) |
Hao, L. S. |
RESEARCH ON MONITORING AND CONTROL SYSTEM BASED PLC IN THE NF-6 WIND TUNNEL |
ICAS2008-P2.10 |
Haraldsdottir, A. |
ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES |
ICAS 2008-11.9.3 (AIAA 2008-8932) |
Hardy, P. |
A NOVEL RECIPROCAL SOUND TRANSMISSION MEASURING METHOD, APPLIED ON A COMPOSITE FUSELAGE |
ICAS 2008-4.9.3 |
Harris, D. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
Hartung, D. |
MECHANICS OF COMPOSITES IN LIGHTWEIGHT STRUCTURES: EFFICIENT TESTING AND COMPUTATION ACCOUNTING FOR COMPLEX 3D BEHAVIOUR |
ICAS 2008-7.11.2 |
Hashimoto, J. -I. |
CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION |
ICAS 2008-1.2.3 |
Hatanaka, K. |
MULTI-DISCIPLINARY DESIGN EXPLORATION FOR WINGLET |
ICAS 2008-1.1.3 |
Haucke, F. |
ACTIVE SEPARATION CONTROL ON A SLATLESS 2D HIGH-LIFT WING SECTION |
ICAS 2008-3.11.2 |
Hauf, T. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
Haupt, M. C. |
NUMERICAL ANALYSIS OF THIN-WALLED STRUCTURES IN HYPERSONIC FLOW REGIME |
ICAS 2008-3.6.1 |
Haupt, M. C. |
NUMERICAL SIMULATION OF AN OSCILLATING AND FLEXIBLE AIRFOIL FOR FLAPPING WING PROPULSION WITH FLUID-STRUCTURE INTERACTION |
ICAS 2008-7.10.4 |
Hayase, T. |
MEASUREMENT OF UNSTEADY AERODYNAMIC FORCES OF 3D FLAPPING WING IN HOVERING TO FORWARD FLIGHT |
ICAS 2008-3.4.3 |
Heatley, D. P |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
Heblij, S. J. |
OPTIMIZATION OF RNAV NOISE ABATEMENT ARRIVAL TRAJECTORIES |
ICAS 2008-4.11.1 |
Heere,, K. |
ALGORITHM AND OPERATIONAL CONCEPT FOR RESOLVING SHORT-RANGE CONFLICTS |
ICAS 2008-8.7.5 |
Heiligers, M. M. |
FEASIBILITY ANALYSIS OF ACHIEVING A STABILIZED APPROACH |
ICAS 2008-5.4.2 |
Heinze, W. |
THE GREEN FREIGHTER PROJECT - OBJECTIVES AND FIRST RESULTS |
ICAS 2008-4.10.3 |
Hellbach, T. |
TOWARDS SESAR PERFORMANCE TARGETS - THE SUPER-HIGHWAY APPROACH |
ICAS 2008-10.10.1 (AIAA 2008-8935) |
Hendrick, P. |
A FLIGHT THRUST DECK FOR THE F100 TURBOFAN OF THE F16 AIRCRAFT |
ICAS 2008-4.5.1 |
Hendrick, P. |
PRELIMINARY DESIGN OF A JOINED WING HALE UAV |
ICAS 2008-1.4.3 |
Henke, R. |
LONG TERM AIRCRAFT PROJECT AND TECHNOLOGY EVALUATION UNDER THE UNCERTAINTY OF FUTURE SCENARIOS |
ICAS 2008-1.3.4 |
Herbiet, J. -F. |
A FLIGHT THRUST DECK FOR THE F100 TURBOFAN OF THE F16 AIRCRAFT |
ICAS 2008-4.5.1 |
Herbin, E. |
UNCERTAINTIES AT THE CONCEPTUAL STAGE: MULTILEVEL MULTIDISCIPLINARY DESIGN AND OPTIMIZATION APPROACH |
ICAS 2008-1.1.2 |
Hering, H. |
FROM ANALOGUE BROADCAST RADIO TOWARDS END-TO-END COMMUNICATION |
ICAS2008-P8.3 (AIAA 2008-8874) |
Heringer, F. M. |
580 A MULTIDISCIPLINARY OPTIMIZATION METHOD APPLIED TO AIRCRAFT DESIGN |
ICAS2008-P1.4 |
Hernandez, S. |
SIZE OPTIMIZATION OF AIRCRAFT STRUCTURES |
ICAS2008-7.11 ST: |
Hernández, S. |
THERMAL DESIGN UNDER UNCERTAINTIES OF AIRCRAFT STRUCTURES |
ICAS 2008-7.2.3 |
Herreria, J. A. |
SAFE AUTOMATIC FLIGHT BACK AND LANDING OF AIRCRAFT (SOFIA) |
ICAS2008-9.7 ST: |
Herszberg, I. |
LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS |
ICAS 2008-7.2.2 |
Hess, D. E. |
SIMULATION OF A NON-AXISYMMETRIC UNDERSEA VEHICLE USING A RECURSIVE NEURAL NETWORK |
ICAS 2008-5.8.2 |
Hesselink, H. H. |
ENVIRONMENT-AWARE RUNWAY ALLOCATION ADVICE SYSTEM |
ICAS 2008-4.11.2 |
Hiernaux, O. |
EVOLUTION OF FUTURE EQUIPMENTS AND SUB-SYSTEMS FOR THE FUTURE GREEN AIRCRAFT |
ICAS 2008-6.4.1 INVITED |
Higuchi, K. |
WING DESIGN OF SUPERSONIC TRANSPORT BY A MULTI-POINT OPTIMIZATION METHOD |
ICAS 2008-2.4.3 |
Hileman, J. I. |
PAYLOAD FUEL ENERGY EFFICIENCY AS A METRIC FOR AVIATION ENVIRONMENTAL PERFORMANCE |
ICAS 2008-4.7.4 |
Hileman, J. I. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
Hirai, K. |
VORTEX BEHAVIORS OF CRANKED ARROW WING CONFIGURATIONS WITH DIFFERENT WING PLANFORMS |
ICAS 2008-3.3.2 |
Hirai, T. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
Hitzel, M. |
AERODYNAMIC OPTIMIZATION OF AIRCRAFT CONFIGURATIONS WITH MULTIDISZIPLINARY ASPECTS |
ICAS 2008-2.11.3 |
Hiyama, J. |
HIGH-ORDER LARGE EDDY SIMULATION AROUND 2-D AEROFOIL WITH HIGH-LIFT DEVICE |
ICAS 2008-2.1.2 |
Hochstetler, R. |
AIRSHIP TRANSPORT OPERATIONAL MANAGEMENT IN NORTHERN LATITUDES |
ICAS 2008-10.1.1 (AIAA 2008-8850) |
Höcht, L. |
TRAJECTORY CONTROL IMPROVEMENT BASED ON A NONLINEAR DYNAMIC INVERSION APPROACH |
ICAS 2008-5.7.2 |
Hoeijmakers, H. W. M. |
NUMERICAL SIMULATION OF ICE ACCRETION ON MULTIPLE-ELEMENT AIRFOIL SECTIONS |
ICAS 2008-2.2.2 |
Hofbauer, K. |
FROM ANALOGUE BROADCAST RADIO TOWARDS END-TO-END COMMUNICATION |
ICAS2008-P8.3 (AIAA 2008-8874) |
Hofbauer, W. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
Hoffman, J. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
Hoffman, R. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
Hoffman, R. |
PRINCIPLES OF AIRSPACE TUBE DESIGN FOR DYNAMIC AIRSPACE CONFIGURATION |
ICAS 2008-10.10.5 (AIAA 2008-8939) |
Hogenhuis, R. H. |
A PRACTICAL APPROACH TO MULTI-OBJECTIVE CAPACITY ANALYSIS OF AN ENVIRONMENT-AWARE AIRPORT |
ICAS 2008-8.5.1 |
Hogenhuis, R. H. |
OPTIMIZATION OF RNAV NOISE ABATEMENT ARRIVAL TRAJECTORIES |
ICAS 2008-4.11.1 |
Holden, T. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
Hollingsworth, P. |
A METHOD FOR ASSESSING THE ENVIRONMENTAL BENEFIT OF FUTURE AVIATION TECHNOLOGIES |
ICAS2008-P10.2 |
Holm, A. H. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
Holmberg, A. |
ROUTE PLANNING FOR RELAY UAV |
ICAS 2008-5.6.2 |
Holmes, B. J. |
IMPLEMENTING NEXT GENERATION AIR TRANSPORTATION SYSTEM TECHNOLOGIES |
ICAS 2008-8.4.3 |
Holsclaw, C. |
GOING GREEN – MITIGATING AVIATION’S NEW ENVIRONMENTAL DRIVERS |
ICAS 2008-4.7.2 |
Holzapfel, F. |
IMPROVEMENT FOR LANDING ON SMALL-MEDIUM AIRPORTS USING FUTURE, AIRCRAFT-AUTONOMOUS GUIDANCE AIDS |
ICAS 2008-5.7.1 INVITED |
Holzapfel, F. |
TRAJECTORY CONTROL IMPROVEMENT BASED ON A NONLINEAR DYNAMIC INVERSION APPROACH |
ICAS 2008-5.7.2 |
Holzapfel, F. |
UNIQUE PERFORMANCE CHARACTERISTICS OF SOLAR AIRCRAFT |
ICAS 2008-5.3.2 |
Holzäpfel, F. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
Holzäpfel, F. |
PERFORMANCE OF THE WAKE VORTEX PREDICTION AND MONITORING SYSTEM WSVBS AT FRANKFURT AIRPORT |
ICAS 2008-8.11.2 |
Holzwarth, R. |
FLIGHT VEHICLE COMPOSITE STRUCTURES |
ICAS 2008-7.9.1 (AIAA 2008-8976 ) |
Homan, J. J. |
THE INFLUENCE OF FATIGUE CRACK INITIATION BEHAVIOUR OF FRICTION STIR WELDED JOINTS ON THE DESIGN CRITERIA |
ICAS 2008-7.6.2 |
Homola, J. |
HUMAN-IN-THE-LOOP EVALUATION OF GROUND-BASED AUTOMATED SEPARATION ASSURANCE FOR NEXTGEN |
ICAS 2008-11.4.5 (AIAA 2008-8885) |
Hong, S.- M. |
15 THE SIGNAL-TO-NOISE RATIO MODELING OF RADAR IN ELECTRONIC COUNTER-COUNTER MEASURES |
ICAS2008-P6.7 |
Hoogendijk, P. L. |
MULTI-DISCIPLINARY INSTALLATION OF THE EAGLE'S EYE |
ICAS2008-P6.9 |
Hook, L. R. |
147 THE LOW DOWN – DIGITAL TERRAIN DATA FOR AUTOMATIC GROUND COLLISION AVOIDANCE |
ICAS2008-P6.10 |
Horinouchi, S. |
NOISE REDUCTION BY THRUST VECTORING FOR SUPERSONIC BUSINESS JET |
ICAS 2008-4.8.3 |
Horn, W. |
"ACTIVE CORE" - A KEY TECHNOLOGY FOR MORE ENVIRONMENTALLY FRIENDLY AERO ENGINES BEING INVESTIGATED UNDER THE NEWAC PROGRAM |
ICAS 2008-4.2.1 |
Horst, P. |
NUMERICAL ANALYSIS OF THIN-WALLED STRUCTURES IN HYPERSONIC FLOW REGIME |
ICAS 2008-3.6.1 |
Horst, P. |
NUMERICAL SIMULATION OF AN OSCILLATING AND FLEXIBLE AIRFOIL FOR FLAPPING WING PROPULSION WITH FLUID-STRUCTURE INTERACTION |
ICAS 2008-7.10.4 |
Horton, G. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Hoseinalipour, S. M. |
EXPERIMENTAL INVESTIGATION OF SPRAY CHARACTERISTICS OF DOUBLE-BASE SWIRL INJECTOR |
ICAS2008-4.1 ST: |
Hospers, J. M. |
NUMERICAL SIMULATION OF ICE ACCRETION ON MULTIPLE-ELEMENT AIRFOIL SECTIONS |
ICAS 2008-2.2.2 |
Howell, D. |
OPERATIONAL ASSESSMENT OF THE INTEGRATED TERMINAL WEATHER SYSTEM (ITWS) USING DIRECT MEASUREMENT |
ICAS 2008-10.7.5 (AIAA 2008-8918) |
Howell, K. M. |
LARGE UAS OPERATIONS IN THE NAS - THE NASA 2007 WESTERN STATES FIRE MISSIONS |
ICAS 2008-8.1.3 (AIAA 2008-8967) |
Howland, M. |
AIRSPACE SECURITY MEASURES EMPLOYED FOR THE UN GENERAL ASSEMBLY MEETING: ANALYSIS AND IMPACT |
ICAS 2008-11.5.1 (AIAA 2008-8892) |
Hsieh, C. H. |
THE IMPLEMENTATION OF ANALYTICAL HIERARCHY PROCESS IN FLIGHT SAFETY |
ICAS 2008-9.2.4 |
Hu, Y. F. |
METHODS FOR CALCULATING THE DAMAGE-RATE OF AIRCRAFT COMPONENT |
ICAS2008-9.8 ST: |
Huang, C. K. |
NUMERICAL SIMULATION OF FLAPPING WING AERODYNAMIC PERFORMANCE UNDER GUST WIND CONDITIONS |
ICAS2008-3.5 ST: |
Huang, P. |
ANALYSIS OF THE SCATTERING CHARACTERISTICS FROM DISCONTINUITY SURFACES ON AIRCRAFT USING A MODIFIED MLFMA |
ICAS2008-P3.6 |
Huang, X. |
SUPPRESSING BOUNDARY LAYER SEPARATION BY UNSTEADY EXCITATION OF MINI-SCALE LEADING-EDGE FLAPS |
ICAS 2008-3.10.1 |
Huber, C. |
STATIC AND FATIGUE ANALYSIS OF AN UPPER WING SKIN WITH EXFOLIATION CORROSION |
ICAS 2008-7.4.1 |
Hübner, N. |
PREPARING LP TURBINE TECHNOLOGY FOR MODERN AIRCRAFT ENGINES |
ICAS 2008-4.6.1 |
Huebsch, W. W. |
CONTROL OF A SWEPT WING TAILLESS AIRCRAFT THROUGH WING MORPHING |
ICAS 2008-2.7.1 |
Hui, K. |
CESSNA CITATION CJ1 FLIGHT TEST DATA GATHERING AND LEVEL-C SIMULATOR MODEL DEVELOPMENT |
ICAS 2008-5.1.2 |
Hummel, D. |
THE SECOND INTERNATIONAL VORTEX FLOW EXPERIMENT (VFE-2): RESULTS OF THE FIRST PHASE 2003 - 2008 |
ICAS 2008-3.3.1 INVITED |
Hunter, G. |
TOWARD AN ECONOMIC MODEL TO INCENTIVIZE VOLUNTARY OPTIMIZATION OF NAS TRAFFIC FLOW |
ICAS 2008-10.4.1 (AIAA 2008-8887) |
Hüttig, G. |
RESEARCH ON INTEGRATED COLLIMATED COCKPIT VISUAL AND FLIGHT INFORMATION SYSTEM |
ICAS 2008-9.10.1 |
Huysseune, J. |
EVOLUTION OF FUTURE EQUIPMENTS AND SUB-SYSTEMS FOR THE FUTURE GREEN AIRCRAFT |
ICAS 2008-6.4.1 INVITED |
Hwang, T. W |
NONLINEAR FORMATION GUIDANCE LAW WITH ROBUST DISTURBANCE OBSERVER |
ICAS 2008-5.7.4 |
Hwang, T. W. |
INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT |
ICAS 2008-5.7.3 |
Ichikawa, G. |
ESTIMATION OF THE INFLUENCE OF PROFILE ERROR ON AERODYNAMIC PERFORMANCE FOR LOW-REYNOLDS-NUMBER AIRFOILS |
ICAS2008-3.7 ST: |
Idris, H. |
TASK ANALYSIS FOR FEASIBILITY ASSESSMENT OF A COLLABORATIVE TRAFFIC FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.7.3 (AIAA 2008-8909) |
Iijima, T. |
CBAQ: DEVELOPMENT OF CRM BEHAVIOR ANALYSIS METHOD FOR MISSION FLIGHT CREW TRAINING |
ICAS 2008-9.2.1 |
Ikeda, T. |
INTERFACE CONDITIONS OF FINITE-DIFFERENCE COMPACT SCHEMES FOR COMPUTATIONAL AEROACOUSTICS |
ICAS 2008-2.3.1 |
Imamura, T. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
Inokuchi, H. |
DEVELOPMENT OF AN ONBOARD DOPPLER LIDAR FOR FLIGHT SAFETY |
ICAS 2008-9.9.2 |
Irving, P. E. |
SIMPLIFYING MSD MODELING BY USING CONTINUING DAMAGE ASSUMPTION AND PARAMETRIC STUDY: THE ROLE OF RIVET SQUEEZE FORCE |
ICAS 2008-9.8.1 |
Isaksson, O. |
VIRTUAL ENTERPRISE COLLABORATION - BREAKTHROUGH TECHNOLOGIES PROVIDED BY VIVACE |
ICAS 2008-8.10.4 INVITED |
Iscold, P. H. A. O. |
DEVELOPMENT OF A SMALL UNMANNED AIR VEHICLE WITH MINIMUM SENSORS PHILOSOPHY |
ICAS2008-1.4 ST: |
Ishikawa, H. |
FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1) |
ICAS 2008-2.4.2 |
Ishikawa, H. |
NUMERICAL STUDY OF A PITOT PROBE WITH FIVE-HOLE PYRAMIDAL HEAD FOR SUPERSONIC FLIGHT TEST |
ICAS 2008-3.2.4 |
Ishutkina, M. A. |
ANALYSIS OF INTERACTION BETWEEN AIR TRANSPORTATION AND ECONOMIC ACTIVITY |
ICAS 2008-10.4.2 (AIAA 2008-8888) |
Isikveren, A. T. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
Isogai, K. |
MEASUREMENT OF UNSTEADY AERODYNAMIC FORCES OF 3D FLAPPING WING IN HOVERING TO FORWARD FLIGHT |
ICAS 2008-3.4.3 |
Isogai, K. |
OPTIMUM AEROELASTIC DESIGN OF A RESONANCE TYPE FLAPPING WING FOR MICRO AIR VEHICLES |
ICAS 2008-7.10.3 |
Israeli, E. R. |
COMPUTATIONAL INVESTIGATION AND DESIGN OF COMPLIANT MEMBRANE WINGS FOR BIOLOGICALLY INSPIRED FLIGHT VEHICLES |
ICAS 2008-2.10.1 |
Ito, K. |
PARAMETRIC STUDY AND MITIGATION OF PORPOISING IN WATERBORN AIRCRAFTS |
ICAS2008-5.8 ST: |
Ito, T. |
AEROACOUSTIC NOISE MEASUREMENTS IN AERODYNAMIC LOW-SPEED WIND TUNNELS |
ICAS 2008-3.2.3 |
Ito, T. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
Ito, T. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
Itoh, E. |
HARMONIZING AUTOMATION, PILOT AND AIR TRAFFIC CONTROLLER IN THE FUTURE AIR TRAFFIC MANAGEMENT |
ICAS 2008-8.2.4 |
Iuso, G. |
LARGE-SCALE MANIPULATION OF A TURBULENT BOUNDARY LAYER BY MEANS OF A 2D SYNTHETIC JET |
ICAS2008-P2.8 |
Iuso, G. |
TRANSVERSAL INJECTED SYNTHETIC JETS FOR WALL TURBULENCE CONTROL |
ICAS 2008-3.10.3 |
Ivanov, M. J. |
UNSTEADY CFD MODELING OF WHOLE GAS TURBINE ENGINE FLOW PASSAGE WITH APPLICATIONS |
ICAS2008-4.4 ST: |
Jacazio, G. |
A DUAL-DUPLEX ELECTROHYDRAULIC SYSTEM FOR THE FLY-BY-WIRE CONTROL OF A HELICOPTER MAIN ROTOR |
ICAS 2008-6.6.4 |
Jackson, C. |
METHODOLOGIES FOR ESTIMATING THE IMPACT OF SEVERE WEATHER ON AIRSPACE CAPACITY |
ICAS 2008-10.7.4 (AIAA 2008-8917) |
Jacobs, S. J. |
NUMERICAL SIMULATION OF ICE ACCRETION ON MULTIPLE-ELEMENT AIRFOIL SECTIONS |
ICAS 2008-2.2.2 |
Jaenker, P. |
PIEZO ACTIVE VIBRATION AND NOISE CONTROL IN HELICOPTERS |
ICAS 2008-4.9.2 INVITED |
Jafari, A. A. |
SCALED DOWN MODELS FOR FREE VIBRATION ANALYSIS OF ORTHOGONALLY STIFFENED CYLINDRICAL SHELLS USING SIMILITUDE THEORY |
ICAS 2008-7.7.5 |
Jahagirdar, Y. P. |
DESIGN, FABRICATION AND OPERATION OF REMOTELY CONTROLLED AIRSHIPS IN INDIA |
ICAS 2008-10.1.3 (AIAA 2008-8853) |
Jahangir, E. |
SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT |
ICAS 2008-11.2.2 (AIAA 2008-8858) |
Jatiningrum, D. |
648 TEST FLYING UNMANNED WISE AS A MEANS FOR PROOF OF CONCEPT |
ICAS2008-P5.7 |
Jenie, S.D. |
648 TEST FLYING UNMANNED WISE AS A MEANS FOR PROOF OF CONCEPT |
ICAS2008-P5.7 |
Jenks, M. |
THE BOEING 787 DREAMLINER PROGRAMME |
ICAS 2008-0.8 |
Jeon, K. -S. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
Jia, X. H. |
CFD RESEARCH FOR AIR-TO-AIR MISSILE WITH LATERAL JET CONTROL |
ICAS2008-2.64 ST: |
Jimenez, H. |
TECHNOLOGY-ENABLED IMPROVEMENTS FOR TERMINAL AREA CAPACITY AND ENVIRONMENTAL IMPACT |
ICAS 2008-4.11.3 |
Jin, Y. |
AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH |
ICAS 2008-10.3.1 (AIAA 2008-8861) |
Johansson, T. G |
EVALUATION OF THE FLOW IN AN INTERMEDIATE TURBINE DUCT AT OFF-DESIGN CONDITIONS |
ICAS 2008-4.6.2 |
Johnson, E. |
POTENTIAL ACTIVE-VISION CONTROL SYSTEMS FOR UNMANNED AIRCRAFT |
ICAS 2008-6.8.2 INVITED |
Johnson, N. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
Johnson, W. J. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
Johnston, R. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
Jonas, M. |
MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION |
ICAS 2008-1.5.2 |
Jones, J. |
DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS |
ICAS 2008-6.7.4 |
Jones, K. M. |
OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM |
ICAS 2008-11.6.1 (AIAA 2008-8898) |
Jones, K. M. |
PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY |
ICAS 2008-10.5.2 (AIAA 2008-8896) |
Jouaillec, F. |
THE REGIONAL AEROSPACE CLUSTER POLICY IN EUROPE |
ICAS 2008-6.9.2 |
Jouannet, C. |
AIRCRAFT CONCEPTUAL DESIGN AUTOMATION |
ICAS 2008-1.8.1 |
Joulia, A. |
INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS |
ICAS 2008-8.4.5 |
Judas, M. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
Juhász, A. |
FEASIBILITY STUDY ON MULTI-PHASE FLOW SIMULATION OF FUEL INJECTION USING LATTICE BOLTZMANN METHOD |
ICAS 2008-4.3.4 |
Jump, M. |
BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS |
ICAS 2008-9.10.4 |
Jung, Y. |
AN OPTIMIZATION MODEL FOR REDUCING AIRCRAFT TAXI TIMES AT THE DALLAS-FORT WORTH INTERNATIONAL AIRPORT |
ICAS 2008-8.6.1 |
Jung, Y. |
IMPLICATION OF VARIABILITY IN AIRPORT SURFACE OPERATIONS ON 4-D TRAJECTORY PLANNING |
ICAS 2008-11.11.3 (AIAA 2008-8960) |
Jung, Y. |
IMPROVED PREDICTION OF GATE DEPARTURE TIMES USING PRE-DEPARTURE EVENTS |
ICAS 2008-11.8.1 (AIAA 2008-8919) |
Kageyama, K. |
DESIGN OF OPERATION DATABASE FOR ATM PERFORMANCE ASSESSMENT |
ICAS 2008-8.9.4 |
Kalnins, K. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
Kaltenhäuser, S. |
REAL TIME SIMULATION OF INTEGRATION OF UAV'S INTO AIRSPACE |
ICAS 2008-8.1.1 |
Kamisawa, Y. |
OPTIMUM AEROELASTIC DESIGN OF A RESONANCE TYPE FLAPPING WING FOR MICRO AIR VEHICLES |
ICAS 2008-7.10.3 |
Kamiyoshihara, Y. |
DEVELOPMENT OF THE DISPLAY DEVICE OF POWER DISTIBUTION SYSTEM (DEVELOPMENT OF THE DEPTH FUSED 3-D DISPLAY FOR AIRCRAFT) |
ICAS2008-6.5 ST: |
Kanazaki, M. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
Kang, R. |
THE SYSTEM FAULT BEHAVIOR AND MODEL |
ICAS2008-P9.2 |
Karama, M. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
Kargar Neghab, A. |
EXPERIMENTAL INVESTIGATION OF SPRAY CHARACTERISTICS OF DOUBLE-BASE SWIRL INJECTOR |
ICAS2008-4.1 ST: |
Karl, A. |
DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS |
ICAS 2008-6.7.4 |
Kasai, K. |
ESTIMATION OF THE INFLUENCE OF PROFILE ERROR ON AERODYNAMIC PERFORMANCE FOR LOW-REYNOLDS-NUMBER AIRFOILS |
ICAS2008-3.7 ST: |
Kato, H. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
Kato, H. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
Kato, T. |
RELATION BETWEEN TRAILING EDGE NOISE AND BOUNDARY LAYER INSTABILITY |
ICAS2008-P2.14 |
Katz, J. B. |
PAYLOAD FUEL ENERGY EFFICIENCY AS A METRIC FOR AVIATION ENVIRONMENTAL PERFORMANCE |
ICAS 2008-4.7.4 |
Katzenberger, K.W. |
F/A 18 E/F TOTAL PRODUCTION SYSTEM |
ICAS 2008-6.7.2 |
Kawadu, T. |
DEVELOPMENT OF THE DISPLAY DEVICE OF POWER DISTIBUTION SYSTEM (DEVELOPMENT OF THE DEPTH FUSED 3-D DISPLAY FOR AIRCRAFT) |
ICAS2008-6.5 ST: |
Kawai, M. |
AERODYNAMIC DESIGN AND ITS VALIDATION OF AN OPEN-TYPE ENGINE RUN-UP FACILITY |
ICAS 2008-4.5.3 |
Kawazoe, H. |
FOREBODY VORTEX CONTROL ON HIGH PERFORMANCE AIRCRAFT USING PWM-CONTROLLED PLASMA ACTUATORS |
ICAS 2008-3.3.4 |
Keck, B. |
REAL TIME SIMULATION OF INTEGRATION OF UAV'S INTO AIRSPACE |
ICAS 2008-8.1.1 |
Kelly, P. |
AEROSPACE PRODUCT COST MANAGEMENT AT THE EARLY CONCEPT OPERATIONS PHASE |
ICAS 2008-10.6.2 (AIAA 2008-8904) |
Kennepohl, F. |
PREPARING LP TURBINE TECHNOLOGY FOR MODERN AIRCRAFT ENGINES |
ICAS 2008-4.6.1 |
Kerns, K. |
SAY WHO? PILOTED SIMULATION STUDY OF COMMUNICATIONS CENTERED AROUND A COCKPIT TRAFFIC DISPLAY |
ICAS 2008-10.5.1 (AIAA 2008-8895) |
Khalid, M. |
A CFD STUDY OF UCAV 1303 BASELINE MODEL AT CRUISE MACH NUMBERS |
ICAS 2008-2.5.1 |
Khan, S. U. |
FATIGUE CRACK GROWTH PREDICTION OF FIBRE REINFORCED METAL LAMINATES UNDER VARIABLE AMPLITUDE LOADING |
ICAS 2008-7.6.1 |
Khan, Z. |
MECHANICALLY UNCOUPLED SERVO TABS FOR PRIMARY FLIGHT CONTROLS |
ICAS 2008-5.2.3 |
Khodagolian, V. |
AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS |
ICAS 2008-3.11.3 |
Khosoussi, S. |
FEM MICRO-MECHANICAL ANALYSIS OF DELAMINATION PHENOMENON IN IMC LAMINATED COMPOSITES USING DAMAGE THEORY |
ICAS2008-9.4 ST: |
Khreish, J. |
EVALUATION OF AN INTEROPERABLE VERTICAL TAKE-OFF UAV FOR OPERATIONS WITH UGVS - AN OVERVIEW |
ICAS 2008-6.11.2 |
Khromov, V. |
GROUND EFFECT MODELING FOR ROTARY-WING SIMULATION |
ICAS 2008-5.11.3 |
Khurana, M. S. |
APPLICATION OF AN HYBRID OPTIMIZATION APPROACH IN THE DESIGN OF LONG ENDURANCE AIRFOILS |
ICAS 2008-2.8.2 |
Kielb, R. E. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
Kim, B. |
SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT |
ICAS 2008-11.2.2 (AIAA 2008-8858) |
Kim, B. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Kim, B. J. |
PERFORMANCE EVALUATION AND HILS TEST OF CONTROL ALLOCATION METHODS FOR RECONFIGURATION CONTROL |
ICAS 2008-5.10.3 |
Kim, E. T. |
PERFORMANCE EVALUATION AND HILS TEST OF CONTROL ALLOCATION METHODS FOR RECONFIGURATION CONTROL |
ICAS 2008-5.10.3 |
Kim, J. |
TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.1.1 (AIAA 2008-8854) |
Kim, M. |
BIRD-STRIKE DAMAGE ANALYSIS IN CONCEPT ADVANCED COMPOSITE FAN BLADES |
ICAS 2008-4.4.1 |
Kim, S. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
Kim, T. H |
NONLINEAR FORMATION GUIDANCE LAW WITH ROBUST DISTURBANCE OBSERVER |
ICAS 2008-5.7.4 |
Kim, Y. S. |
OPTIMIZATION FOR FLIGHT CONTROL SYSTEM WITH CONSTRAINTS SUPPLEMENTED HANDLING QUALITIES |
ICAS 2008-5.3.4 |
King, J. |
ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES |
ICAS 2008-11.9.3 (AIAA 2008-8932) |
Kintscher, M. |
ACTIVE AND PASSIVE STRUCTURAL MEASURES FOR AEROELASTIC WINGLET DESIGN |
ICAS 2008-7.10.1 |
Kirby, M. R. |
AN APPROACH FOR VERIFICATION AND VALIDATION OF THE ENVIRONMENTAL DESIGN SPACE |
ICAS2008-P8.4 (AIAA 2008-8875) |
Kirby, M. R. |
THE ENVIRONMENTAL DESIGN SPACE |
ICAS 2008-4.7.3 |
Kladetzke, J. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
Klar, J. U. |
FIN BUFFET CHARACTERISTICS OF ADVANCED TRAINER AIRCRAFT |
ICAS 2008-3.4.1 |
Kling, A. |
COLLAPSE BEHAVIOR OF THIN-WALLED CFRP STRUCTURES DUE TO MATERIAL AND GEOMETRIC NONLINEARITIES–EXPERIMENTS AND SIMULATION |
ICAS 2008-7.11.3 |
Klingauf, U. |
SIMULATOR EVALUATION OF A NOVEL SURFACE MOVEMENT AWARENESS AND ALERTING SYSTEM (SMAAS) FOR RUNWAY INCURSION AVOIDANCE |
ICAS 2008-11.11.2 (AIAA 2008-8959) |
Kloepperl, V. |
PIEZO ACTIVE VIBRATION AND NOISE CONTROL IN HELICOPTERS |
ICAS 2008-4.9.2 INVITED |
Knoerzer, D. |
EUROPE'S RESEARCH TACKLES THE GLOBAL CHALLENGES TO AERONAUTICS |
ICAS 2008-6.9.1 INVITED |
Koenig, R. |
DESIGN OF 4D LANDING APPROACH TRAJECTORIES FOR A QUIET STOL AIRPLANE |
ICAS 2008-4.8.2 |
Koenig, R. |
EVALUATION OF SIMULATOR AND FLIGHT TESTED NOISE ABATEMENT APPROACH PROCEDURES |
ICAS 2008-4.8.1 |
Koenke, E. |
DEVELOPMENT AND APPLICATION OF AN INTEGRATED APPROACH TOWARD NASA AIRSPACE SYSTEMS RESEARCH |
ICAS 2008-10.8.1 (AIAA 2008-8924) |
Koepf, A. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
Kohama, Y. |
RELATION BETWEEN TRAILING EDGE NOISE AND BOUNDARY LAYER INSTABILITY |
ICAS2008-P2.14 |
Kokkalis, A. |
AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS |
ICAS 2008-3.11.3 |
Konishi, Y. |
RELATION BETWEEN TRAILING EDGE NOISE AND BOUNDARY LAYER INSTABILITY |
ICAS2008-P2.14 |
Konrath, R. |
DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS |
ICAS 2008-3.2.1 |
Konstanzer, P. |
PIEZO ACTIVE VIBRATION AND NOISE CONTROL IN HELICOPTERS |
ICAS 2008-4.9.2 INVITED |
Kontis, K. |
THE INVESTIGATION OF DEPENDENCE OF LOW FREQUENCY MOTION ON UPSTREAM FLOW CONDITIONS IN HYPERSONIC FLOWS |
ICAS2008-3.7 ST: |
Kopardekar, P. |
RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY |
ICAS 2008-8.2.3 |
Korn, B. |
PERFORMANCE-BASED TMA HANDLING FOR MIXED TRAFFIC USING A GROUND BASED 4D-GUIDANCE FOR UNEQUIPPED AIRCRAFT |
ICAS 2008-10.8.3 |
Kos, J. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
Kotegawa, T. |
UTILIZATION OF NETWORK THEORY FOR THE ENHANCEMENT OF ATO AIR ROUTE FORECAST |
ICAS 2008-11.10.5 (AIAA 2008-8944) |
Kowalczyk, G. |
FLIGHT SAFETY AS CONSIDERED IN PROBABILISTIC TERMS |
ICAS 2008-9.3.4 |
Kowalczyk, G. |
MODELING AND SIMULATION OF FLAPPING WINGS MICRO-AERIAL VEHICLES FLIGHT DYNAMICS |
ICAS 2008-5.9.1 INVITED |
Kroo, I. M. |
MULTI-OBJECTIVE AIRCRAFT OPTIMIZATION FOR MINIMUM COST AND EMISSIONS OVER SPECIFIC ROUTE NETWORKS |
ICAS 2008-10.6.3 (AIAA 2008-8905) |
Kroo, I. M. |
THEORETICAL AND EXPERIMENTAL INVESTIGATION OF ENERGY EXTRACTION FROM ATMOSPHERIC TURBULENCE |
ICAS2008-1.5 ST: |
Krozel, J. |
CAUSALITY ANALYSIS FOR AVIATION WEATHER HAZARDS |
ICAS 2008-10.7.1 (AIAA 2008-8914) |
Krozel, J. |
ON-DEMAND SPECIAL USE AIRSPACE |
ICAS 2008-10.10.4 (AIAA 2008-8938) |
Krozel, J. |
TASK ANALYSIS FOR FEASIBILITY ASSESSMENT OF A COLLABORATIVE TRAFFIC FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.7.3 (AIAA 2008-8909) |
Krüger, J. |
FLIGHT SIMULATORS – ON DIFFERENT PERCEPTIONS OF MANUFACTURERS, AVIATION AUTHORITIES, RESEARCH AND USERS |
ICAS 2008-5.5.1 INVITED |
Krus, P. |
A QUANTIFIED RELATIONSHIP MATRIX AIDED BY PROBABILISTIC DESIGN AND OPTIMIZATION |
ICAS 2008-6.2.1 |
Krus, P. |
AIRCRAFT CONCEPTUAL DESIGN AUTOMATION |
ICAS 2008-1.8.1 |
Krus, P. |
COMPUTATIONAL TOOLS FOR AIRCRAFT SYSTEM ANALYSIS AND OPTIMIZATION |
ICAS 2008-1.8.2 |
Krus, P. |
HOSTED SIMULATION FOR HETEROGENEOUS AIRCRAFT SYSTEM DEVELOPMENT |
ICAS2008-6.2 ST: |
Kubinyi, M. |
EMAT APPLIED IN THE AVIATION INDUSTRY |
ICAS2008-P1.1 (AIAA 2008-8870) |
Kubo, D. |
AUTONOMOUS AERIAL OBSERVATION SYSTEM FOR DISASTER RESPONSE USING ELECTRIC DUCTED FAN MAVS |
ICAS 2008-1.4.5 |
Kubo, D. |
ROBUST OPTIMAL DESIGN OF AN AUTOPILOT FOR TRANSITIONAL FLIGHTS OF A TAIL-SITTER MINI UAV |
ICAS 2008-5.9.2 |
Kuenz, A. |
PERFORMANCE-BASED TMA HANDLING FOR MIXED TRAFFIC USING A GROUND BASED 4D-GUIDANCE FOR UNEQUIPPED AIRCRAFT |
ICAS 2008-10.8.3 |
Kuhlmann, A. |
IMPACT OF ESTOL CAPABILITY ON RUNWAY CAPACITY - AN ANALYTICAL APPROACH |
ICAS 2008-11.9.4 (AIAA 2008-8933) |
Kulemin, A. V. |
ESTIMATION OF CRACK TURN PHENOMENON |
ICAS 2008-7.6.3 |
Kulkarni, D. |
PREDICTION OF WEATHER-RELATED DELAYS IN THE CONTINENTAL UNITED STATES |
ICAS 2008-8.2.2 |
Kumano, T. |
LOW-BOOM AND LOW-DRAG OPTIMIZATION FOR THE TWIN-ENGINE SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR |
ICAS 2008-2.4.1 |
Kunin, A. |
PULSATING COMBUSTION OF AN ORGANIC GEL-FUEL DROPLET AND ITS INFLUENCE ON THE THERMAL FIELD OF A SPRAY DIFFUSION FLAME |
ICAS 2008-4.1.2 |
Kupfer, M. |
AUTOMATED CONFLICT RESOLUTION - A SIMULATION-BASED SENSITIVITY STUDY OF AIRSPACE AND DEMAND |
ICAS 2008-8.9.1 |
Kuratani, N. |
EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE |
ICAS 2008-3.7.5 |
Kuratani, N. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
Kuroda, F. |
NUMERICAL STUDY OF A PITOT PROBE WITH FIVE-HOLE PYRAMIDAL HEAD FOR SUPERSONIC FLIGHT TEST |
ICAS 2008-3.2.4 |
Kurotaki, T. |
HIGH-ORDER LARGE EDDY SIMULATION AROUND 2-D AEROFOIL WITH HIGH-LIFT DEVICE |
ICAS 2008-2.1.2 |
Kurotaki, T. |
INTERFACE CONDITIONS OF FINITE-DIFFERENCE COMPACT SCHEMES FOR COMPUTATIONAL AEROACOUSTICS |
ICAS 2008-2.3.1 |
Kurotaki, T. |
LARGE EDDY SIMULATION AROUND 2-D AIRFOIL WITH NATURAL TRANSITION AT HIGH REYNOLDS NUMBERS |
ICAS2008-2.1 ST: |
Kuzminski, P. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
Kwak, D. Y. |
FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1) |
ICAS 2008-2.4.2 |
Kwak, D. Y. |
NUMERICAL STUDY OF A PITOT PROBE WITH FIVE-HOLE PYRAMIDAL HEAD FOR SUPERSONIC FLIGHT TEST |
ICAS 2008-3.2.4 |
Kwak, D. Y. |
VORTEX BEHAVIORS OF CRANKED ARROW WING CONFIGURATIONS WITH DIFFERENT WING PLANFORMS |
ICAS 2008-3.3.2 |
Kwan, J. S. |
MODEL-BASED AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.1 (AIAA 2008-8907) |
La Rocca, G. |
CONTROLLABILITY OF BLENDED WING BODY AIRCRAFT |
ICAS 2008-5.4.3 |
La Rocca, G. |
KNOWLEDGE BASED ENGINEERING TO SUPPORT AIRCRAFT MULTIDISCIPLINARY DESIGN AND OPTIMISATION |
ICAS 2008-6.10.1 |
Laban, M. |
OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION |
ICAS 2008-2.11.2 |
Lagu, A. V. |
A SYSTEM SAFETY FRAMEWORK FOR ANALYZING FUTURE AIR TRANSPORTATION SEPARATION ASSURANCE AND COLLISION AVOIDANCE CONCEPTS |
ICAS 2008-11.4.3 (AIAA 2008-8883) |
Lai, J. C. S. |
FLAPPING-WING TECHNOLOGY: THE POTENTIAL FOR AIR VEHICLE PROPULSION AND AIRBORNE POWER GENERATION |
ICAS 2008-1.5.1 |
Landry, S. J. |
A SYSTEM SAFETY FRAMEWORK FOR ANALYZING FUTURE AIR TRANSPORTATION SEPARATION ASSURANCE AND COLLISION AVOIDANCE CONCEPTS |
ICAS 2008-11.4.3 (AIAA 2008-8883) |
Langhans, S. |
A HOLISTIC APPROACH TO EVALUATE THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-8.4.2 |
Lanier, R. C. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
Larocca, F. |
EULER INVERSE THROUGHFLOW MODEL BASED ON AN IMPLICIT UPWIND TIME MARCHING TECHNIQUE |
ICAS 2008-2.3.2 |
Laroche, P. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
Laschka, B. |
SMALL DISTURBANCE NAVIER-STOKES COMPUTATIONS FOR LOW ASPECT RATIO WING PITCHING OSCILLATIONS |
ICAS 2008-2.10.3 |
Lauderdale, T. A. |
PREDICTIVE MODELS OF THE NATIONAL AIRSPACE SYSTEM USING BAYESIAN NETWORKS |
ICAS 2008-8.4.4 |
Lavelle, T. |
COUPLED HIGH-FIDELITY ENGINE SYSTEM SIMULATION |
ICAS 2008-8.10.3 INVITED |
Lawson, C. P. |
DESIGN AND DEVELOPMENT OF THE ECLIPSE AND DEMON DEMONSTRATOR UAVS |
ICAS 2008-1.4.2 |
Lawson, C. P. |
THE STATE-OF-THE-ART AND THE FUTURE OF WATER MANAGEMENT WITHIN FUEL TANKS |
ICAS2008-6.4 ST: |
Lawson, C. P. |
THERMAL MANAGEMENT OF ELECTROMECHANICAL ACTUATION ON AN ALL-ELECTRIC AIRCRAFT |
ICAS 2008-6.6.2 |
Le Tallec, C. |
INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS |
ICAS 2008-8.4.5 |
Lee, B. |
THEORETICAL APPROACH TO DIRECTIONAL CONTROL SENSITIVITY SELECTION |
ICAS 2008-5.4.1 INVITED |
Lee, D. |
AVIATION CLIMATE IMPACT - A SUMMARY OF ONGOING EUROPEAN RESEARCH PROGRAMMES |
ICAS 2008-0.3 |
Lee, D. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Lee, J. |
SIMULATION OF A NON-AXISYMMETRIC UNDERSEA VEHICLE USING A RECURSIVE NEURAL NETWORK |
ICAS 2008-5.8.2 |
Lee, J. H. |
DESIGN AND OPERATION OF THE ADD ENVIRONMENTAL TEST FACILITY |
ICAS2008-P6.6 |
Lee, J. -W. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
Lee, K. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
Lee, P. U. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
Lee, S. |
UNSTEADY AERODYNAMIC ANALYSIS OF HELICOPTER ROTOR BY USING THE TIME-DOMAIN PANEL METHOD |
ICAS2008-2.10 ST: |
Lefebvre, T. |
AERODYNAMIC AND AERO-ACOUSTIC DESIGN OF MODERN TILT-ROTORS: THE ONERA EXPERIENCE |
ICAS 2008-1.7.4 |
Legge, J. |
DEPARTURE TAXI TIME PREDICTIONS USING ASDE-X SURVEILLANCE DATA |
ICAS 2008-11.11.1 (AIAA 2008-8958) |
Lehmann, O. |
RESEARCH ON INTEGRATED COLLIMATED COCKPIT VISUAL AND FLIGHT INFORMATION SYSTEM |
ICAS 2008-9.10.1 |
Lehner, S. |
COMBINATORIAL OPTIMIZATION TO INCLUDE GREENER TECHNOLOGIES IN A SHORT-TO-MEDIUM RANGE COMMERCIAL AIRCRAFT |
ICAS 2008-4.10.2 (AIAA 2008-8963) |
Lei, Z. |
WING DESIGN OF SUPERSONIC TRANSPORT BY A MULTI-POINT OPTIMIZATION METHOD |
ICAS 2008-2.4.3 |
Leijonhufvud, M. C. |
DYNAMIC SIMULATION OF A TOWED DECOY SYSTEM |
ICAS 2008-5.11.1 |
Lemmen, H. J. K. |
THE INFLUENCE OF FATIGUE CRACK INITIATION BEHAVIOUR OF FRICTION STIR WELDED JOINTS ON THE DESIGN CRITERIA |
ICAS 2008-7.6.2 |
Lemmers, A. J. J. |
THREAT ASSESSMENT AND RESPONSE MANAGEMENT SYSTEM TARMS: AN ON-BOARD AIRCRAFT SECURITY SYSTEM |
ICAS 2008-9.1.2 |
Lemoine, M. |
THE IMPACT OF RIGOROUS METHODS ON AERONAUTICAL REGULATIONS |
ICAS 2008-9.7.1 |
Lempia, D. |
USING LEAN PRINCIPLES AND MBE IN DESIGN AND DEVELOPMENT OF AVIONICS EQUIPMENT AT ROCKWELL COLLINS |
ICAS 2008-6.7.3 |
Lenz, H. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
Lenz, H. |
GENERATION OF HIGH ACCURATE 4D TRAJECTORIES FOR TAKE-OFF AND DEPARTURE |
ICAS2008-8.11 ST: |
Lenz, J. |
UNIQUE PERFORMANCE CHARACTERISTICS OF SOLAR AIRCRAFT |
ICAS 2008-5.3.2 |
Leuckert, J. |
DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS |
ICAS 2008-3.2.1 |
Levin, K. |
INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.10.1 (AIAA 2008-8940) |
Levy, B. |
DEPARTURE TAXI TIME PREDICTIONS USING ASDE-X SURVEILLANCE DATA |
ICAS 2008-11.11.1 (AIAA 2008-8958) |
Lewe, J. -H. |
ADVANCED GENERAL AVIATION DESIGN WITH TRANSPORTATION ARCHITECTURE ANALYSIS |
ICAS 2008-1.9.4 (AIAA 2008-8929) |
Lewe, J. -H. |
DEMAND-CENTRIC ANALYSIS OF THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-10.4.3 (AIAA 2008-8889) |
Lewitowicz, J. |
MODELING AND SIMULATION OF FLAPPING WINGS MICRO-AERIAL VEHICLES FLIGHT DYNAMICS |
ICAS 2008-5.9.1 INVITED |
Lewitowicz, J. L. |
FLIGHT SAFETY AS CONSIDERED IN PROBABILISTIC TERMS |
ICAS 2008-9.3.4 |
Lhommeau, T. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
Li, A. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
Li, B. F. |
COORDINATELY MODELING AND SIMULATION OF THE EJECTION SEAT/OCCUPANT SYSTEM |
ICAS2008-P9.3 |
Li, D. |
AN APPROXIMATION METHOD FOR THE NUMERICAL SIMULATION ON UNSTEADY FLOWS AROUND SMALL-DISPLACEMENT MOVING OBJECTS |
ICAS2008-3.9 ST: |
Li, D. |
LIFT PREDICTION OF MULTI-ELEMENT AIRFOIL USING DES AND RANS |
ICAS2008-P2.5 |
Li, G. |
TEST DATA MANAGEMENT FOR AIRCRAFT HYDRAULIC SYSTEM TESTING |
ICAS2008-P6.3 |
Li, H. C. H. |
LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS |
ICAS 2008-7.2.2 |
Li, J. S. |
NEW METHOD TO ENHANCE THE WEARABILITY OF TITANIUM ALLOY ROTOR BLADE FOR AERO-ENGINE |
ICAS 2008-4.2.4 |
Li, M. |
MISSION DECISION-MAKING METHOD OF MULTI-AIRCRAFT COOPERATIVELY ATTACKING MULTI-TARGET BASED ON SITUATIONAL ASSESSMENT |
ICAS2008-P1.2 |
Li, M. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
Li, M. |
SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-9.1.3 |
Li, W. |
MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL DEVELOPMENT USING GENETIC ALGORITHM |
ICAS 2008-1.1.1 |
Li, W. J. |
A NEW EFFICIENT INTERACTIVE MULTI-OBJECTIVE EVOLUTIONARY OPTIMIZATION ALGORITHM AND APPLICATION IN ENGINEERING |
ICAS2008-6.2 ST: |
Li, Y. |
AN APPROACH FOR MULTI-CRITERIA DECISION MAKING METHOD SELECTION AND DEVELOPMENT |
ICAS 2008-1.3.1 |
Li, Z. |
EXTENDING FMC TEST FOR FLIGHT SIMULATION AND FLIGHT EXPERIMENTS |
ICAS 2008-5.5.3 |
Li, Z. S. |
DEVELOPMENT OF FLIGHT CONTROL SYSTEM USING EMBEDDED COMPUTER PC-104 |
ICAS2008-P5.1 |
Liang, X. G. |
CFD RESEARCH FOR AIR-TO-AIR MISSILE WITH LATERAL JET CONTROL |
ICAS2008-2.64 ST: |
Liang, Y. M. |
NEW METHOD TO ENHANCE THE WEARABILITY OF TITANIUM ALLOY ROTOR BLADE FOR AERO-ENGINE |
ICAS 2008-4.2.4 |
Liao, M. |
STATIC AND FATIGUE ANALYSIS OF AN UPPER WING SKIN WITH EXFOLIATION CORROSION |
ICAS 2008-7.4.1 |
Lijewski, L. |
IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT |
ICAS 2008-2.6.2 |
Lim, K. M. |
THE STATE-OF-THE-ART AND THE FUTURE OF WATER MANAGEMENT WITHIN FUEL TANKS |
ICAS2008-6.4 ST: |
Lin, G. P. |
A LAYER PAVEMENT MODEL TO SIMULATE ROUGHNESS FEATURES IN ICE ACCRETION NUMERICAL SIMULATION |
ICAS 2008-2.6.1 |
Lin, K. Y. |
PROBABILISTIC MODELING OF STRUCTURAL / AEROELASTIC LIFE CYCLE FOR RELIABILITY EVALUATION OF DAMAGE TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.1.1 |
Lind, I. |
HOSTED SIMULATION FOR HETEROGENEOUS AIRCRAFT SYSTEM DEVELOPMENT |
ICAS2008-6.2 ST: |
Lindberg, A. |
DYNAMIC SIMULATION OF A TOWED DECOY SYSTEM |
ICAS 2008-5.11.1 |
Lindberg, A. |
TRANSONIC STORE SEPARATION STUDIES ON THE SAAB GRIPEN AIRCRAFT USING COMPUTATIONAL AERODYNAMICS |
ICAS 2008-2.9.1 |
Lindeblad, M. |
VIRTUAL ENTERPRISE COLLABORATION - BREAKTHROUGH TECHNOLOGIES PROVIDED BY VIVACE |
ICAS 2008-8.10.4 INVITED |
Lindell, H. |
GRIPEN, PROGRAM OVERVIEW AND FUTURE DEVELOPMENT |
ICAS 2008-1.7.5 |
Lindholm, T. |
CAUSALITY ANALYSIS FOR AVIATION WEATHER HAZARDS |
ICAS 2008-10.7.1 (AIAA 2008-8914) |
Lintelman, S. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
Liscouet, J. |
AUTOMATED GENERATION, SELECTION AND EVALUATION OF ARCHITECTURES FOR ELECTROMECHANICAL ACTUATORS |
ICAS 2008-6.6.1 |
Liscouët-Hanke, S. |
A SIMULATION FRAMEWORK FOR AIRCRAFT POWER SYSTEMS ARCHITECTING |
ICAS 2008-6.2.4 |
Littman, D. |
TOWARD AN ECONOMIC MODEL TO INCENTIVIZE VOLUNTARY OPTIMIZATION OF NAS TRAFFIC FLOW |
ICAS 2008-10.4.1 (AIAA 2008-8887) |
Liu, F. |
NUMERICAL RESEARCHES ON THE AEROELASTIC PROBLEM OF TURBOMACHINERY |
ICAS 2008-4.4.4 |
Liu, H. |
AN UPDATING PROGRAM FOR UNDERGRADUATE AIRCRAFT CONCEPTUAL AND PRELIMINARY DESIGN COURSE |
ICAS2008-P1.5 |
Liu, J. |
FATIGUE BEHAVIOR AND LIFE PREDICTION OF WELDED TITANIUM ALLOY JOINTS |
ICAS 2008-7.4.4 |
Liu, W. T. |
3 A STUDY ON FATIGUE SCATTER FACTOR OF INDIVIDUAL AIRCRAFT STRUCTURE |
ICAS2008-P3.1 |
Liu, Y. |
RESEARCH ON CONTROL ALLOCATION FOR AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS |
ICAS 2008-5.2.4 |
Liu, Y. |
RESEARCH ON FUZZY LOGIC PIO DETECTOR |
ICAS 2008-5.4.5 |
Liu, Z. |
AERODYNAMICS CHARACTERISTICS OF HYPERSONIC VEHICLE IN NEAR SPACE |
ICAS2008-2.5 ST: |
Liu, Z. |
ANALYSIS OF THE SCATTERING CHARACTERISTICS FROM DISCONTINUITY SURFACES ON AIRCRAFT USING A MODIFIED MLFMA |
ICAS2008-P3.6 |
Livne, E. |
PROBABILISTIC MODELING OF STRUCTURAL / AEROELASTIC LIFE CYCLE FOR RELIABILITY EVALUATION OF DAMAGE TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.1.1 |
Lock, G. |
AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF LOW RE NUMBER TRANSITIONAL FLOWS OVER AN AEROFOIL WITH LEADING EDGE SLAT |
ICAS2008-P2.1 (AIAA 2008-8877) |
Lohr, G. |
INFORMATION REQUIREMENTS FOR SUPERVISORY AIR TRAFFIC CONTROLLERS IN SUPPORT OF A MID-TERM WAKE VORTEX DEPARTURE SYSTEM |
ICAS 2008-8.11.3 |
Lohr, G. |
WAKE TURBULENCE MITIGATION FOR ARRIVALS (WTMA) |
ICAS 2008-9.9.3 |
Lombaerts, T. J. J. |
A SIMULATION BENCHMARK FOR AIRCRAFT SURVIVABILITY ASSESSMENT |
ICAS 2008-9.3.2 |
Lopez Ruiz, E. R. |
THE IMPACT OF RIGOROUS METHODS ON AERONAUTICAL REGULATIONS |
ICAS 2008-9.7.1 |
Lourencao, P. T. M. |
EVOLUTION OF EMBRAER’S CIVIL AIRCRAFT |
ICAS 2008-1.7.1 INVITED |
Lozito, S. |
FLIGHT DECK PROCEDURAL GUIDELINES FOR DATALINK TRAJECTORY NEGOTIATIONS |
ICAS 2008-11.6.4 (AIAA 2008-8901) |
Lozito, S. |
PRELIMINARY GUIDELINES ON FLIGHT DECK PROCEDURES FOR VERY CLOSELY SPACED PARALLEL APPROACHES |
ICAS 2008-8.5.2 |
Lu, G. Z. |
INTEGRATED PREDICTION OF MACROSCOPIC PROPERTIES OF COMPOSITES BASED ON FINITE ELEMENT COMPUTATIONAL MICROMECHANICS |
ICAS2008-7.9 ST: |
Lu, S. L. |
INTEGRATED PREDICTION OF MACROSCOPIC PROPERTIES OF COMPOSITES BASED ON FINITE ELEMENT COMPUTATIONAL MICROMECHANICS |
ICAS2008-7.9 ST: |
Lu, Y. |
INTEGRATED PREDICTION OF MACROSCOPIC PROPERTIES OF COMPOSITES BASED ON FINITE ELEMENT COMPUTATIONAL MICROMECHANICS |
ICAS2008-7.9 ST: |
Luan, Y. C. |
THE SIMULATION OF THE HUMAN-MACHINE PARTNERSHIP IN UCAV OPERATION |
ICAS 2008-9.10.5 |
Luber, G. |
APPLICATION OF PVDF FOILS FOR THE MEASUREMENTS OF UNSTEADY PRESSURES ON WIND TUNNEL MODELS FOR THE PREDICTION OF AIRCRAFT VIBRATIONS |
ICAS 2008-3.4.2 |
Luckner, R. |
PILOTED SIMULATION RESULTS OF AN ONBOARD WAKE VORTEX DETECTION, WARNING AND AVOIDANCE SYSTEM AND COCKPIT DISPLAY ASPECTS |
ICAS 2008-9.9.1 |
Ludwig, T. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
Luks, N. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
Lundström, D. |
RAVEN – A SUBSCALE RADIO CONTROLLED BUSINESS JET DEMONSTRATOR |
ICAS 2008-5.5.2 |
Lung, S. -F. |
STRUCTURAL MODEL TUNING CAPABILITY IN AN OBJECT-ORIENTED MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL |
ICAS 2008-9.5.1 |
Lunnon, B. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
Lunsford, C. R. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
Luxhoj, J. T. |
HAZARD, SAFETY RISK AND UNCERTAINTY MODELING OF THE INTEGRATION OF UNMANNED AIRCRAFT SYSTEMS INTO THE NATIONAL AIRSPACE |
ICAS 2008-9.7.2 |
Lv, M. |
THE APPLICATION OF AIRBORNE VIDEO TECHNOLOGIES DURING AERIAL REFUELING TEST |
ICAS2008-P5.2 |
Lyrsell, O. |
A STUDY OF AN USER AND ENVIRONMENTAL FRIENDLY STORED ENERGY BASED EPU/APU-SYSTEM FOR MILITARY AEROSPACE APPLICATIONS |
ICAS 2008-6.4.5 |
Maciel, E. S. de Góes |
SOLUTIONS OF INVISCID AND VISCOUS FLOWS USING STRUCTURED HIGH RESOLUTION ALGORITHMS IN THREE-DIMENSIONS |
ICAS2008-P2.7 |
Macke, O. |
DESIGN OF 4D LANDING APPROACH TRAJECTORIES FOR A QUIET STOL AIRPLANE |
ICAS 2008-4.8.2 |
Macke, O. |
EVALUATION OF SIMULATOR AND FLIGHT TESTED NOISE ABATEMENT APPROACH PROCEDURES |
ICAS 2008-4.8.1 |
MacWilliams, P. V. |
TERMINAL AREA REQUIRED TIME OF ARRIVAL (RTA) CONCEPT OF OPERATIONS AND AUTOMATION PROTOTYPE |
ICAS 2008-11.9.1 (AIAA 2008-8930) |
Maeng, J. S. |
UNSTEADY PROPULSIVE CHARACTERISTICS OF BIOFOILS MOVING IN A VERY LOW-REYNOLDS NUMBER FLOW |
ICAS 2008-3.9.3 |
Magyarits, S. |
RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY |
ICAS 2008-8.2.3 |
Maidl, M. |
SECURITY ARCHITECTURE AND FORMAL ANALYSIS OF AN AIRPLANE SOFTWARE DISTRIBUTION SYSTEM |
ICAS 2008-9.1.1 |
Maier, R. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
Maier, R. |
PIEZO ACTIVE VIBRATION AND NOISE CONTROL IN HELICOPTERS |
ICAS 2008-4.9.2 INVITED |
Maisto, U. |
SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION |
ICAS 2008-2.7.3 |
Makida, M. |
DEVELOPMENT OF FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT JET ENGINE IN JAXA TECHCLEAN PROJECT |
ICAS 2008-4.3.2 |
Malbéqui, P. |
A NOVEL APPROACH TO AIR TRANSPORT SYSTEM ENVIRONMENTAL IMPACT EVALUATION THROUGH PHYSICAL MODELLING AND SIMULATION |
ICAS2008-8.3 ST: |
Malis, M. |
INNOVATIVE COMPOSITE STRUCTURES FOR SMALL AIRCRAFT |
ICAS2008-7.3 ST: |
Malone-Lee, J. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
Malwitz, A. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Mamou, M. |
COMPUTATIONAL FLUID DYNAMICS AND EXPERIMENTAL INVESTIGATION OF AIRPLANE STALL DYNAMICS WITH WING CONTAMINATION |
ICAS 2008-3.5.2 |
Mandanis, G. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
Mane, M. |
BASE OF OPERATIONS CONCEPT FOR ON-DEMAND OPERATIONS |
ICAS 2008-8.6.4 (AIAA 2008-8977 ) |
Mane, M. |
CONCURRENT AIRCRAFT DESIGN AND RESOURCE ALLOCATION UNDER UNCERTAINTY FOR ON-DEMAND AIR TRANSPORTATION |
ICAS 2008-10.6.1 (AIAA 2008-8903) |
Mani, M. |
A HYBRID, DYNAMIC LARGE EDDY SIMULATION METHOD |
ICAS 2008-2.1.1 |
Manipurath, S. |
DEVELOPMENT OF AN INDUSTRIAL SCALE COMBUSTION TEST AND RESEARCH FACILITY FOR ALTERNATIVE FUELS AND FUEL FLEXIBILITY DEMONSTRATION |
ICAS 2008-4.3.1 |
Mansouri, G. |
HEALTH MONITORING FOR COMMERCIAL AIRCRAFT SYSTEMS |
ICAS 2008-6.1.2 |
Mantegazza, P. |
DEVELOPMENT AND VALIDATION OF AN INVESTIGATION TOOL FOR NONLINEAR AEROELASTIC ANALYSIS |
ICAS 2008-9.6.3 |
Mantilla, J. G. |
PAYLOAD FUEL ENERGY EFFICIENCY AS A METRIC FOR AVIATION ENVIRONMENTAL PERFORMANCE |
ICAS 2008-4.7.4 |
Manzato, D. |
A NEW AIRCRAFT CONCEPT: THE COMBAT MALE |
ICAS 2008-1.4.4 |
Marcotte, D. |
FLIGHT EVALUATION OF A COMPACT AIRBORNE TRACE GAS ANALYSIS SENSOR PROOF-OF-CONCEPT |
ICAS2008-P6.4 |
Maré, J.-C. |
AUTOMATED GENERATION, SELECTION AND EVALUATION OF ARCHITECTURES FOR ELECTROMECHANICAL ACTUATORS |
ICAS 2008-6.6.1 |
Marinkovski, D. |
APPLICATION OF SEMICONDUCTOR STRAIN GAUGES IN MEASUREMENTS OF DYNAMIC STABILITY DERIVATIVES IN THE T-38 WIND TUNNEL |
ICAS 2008-3.4.5 |
Marissen, R. |
CARBON/DYNEEMA INTRALAMINAR HYBRIDS: NEW STRATEGY TO INCREASE IMPACT RESISTANCE OR DECREASE MASS OF CARBON FIBER COMPOSITES |
ICAS 2008-7.3.4 |
Markovic, D. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
Maroney, D. |
NEXTGEN AND SESAR: OPPORTUNITIES FOR UAS INTEGRATION |
ICAS 2008-10.8.2 (AIAA 2008-8925) |
Marques, F. D. |
AERO-STRUCTURAL MDO OF A SPAR-TANK-TYPE WING FOR AIRCRAFT CONCEPTUAL DESIGN |
ICAS2008-1.1 ST: |
Marques, F. D. |
DYNAMIC ANALYSIS OF AEROELASTIC RESPONSE FOR TRANSONIC FLOW WITH NONLINEAR STRUCTURAL MODEL |
ICAS 2008-9.6.4 |
Marques, J. M. G. |
ON THE MINIMIZATION OF CRUISE DRAG DUE TO PITCH TRIM FOR A FLYING-WING CONFIGURATION |
ICAS 2008-5.3.3 |
Marques, J. M. G. |
ON THE PROBABILITY OF COLLISION FOR CLIMBING AND DESCENDING TRAJECTORIES RELEVANT TO AIR TRAFFIC MANAGEMENT |
ICAS2008-9.3 ST: |
Marsden, A. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
Martin, C. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
Martinez-Val, R. |
AIRPLANE DESIGN: A MUST IN AERONAUTICAL ENGINEERING EDUCATION |
ICAS2008-P1.6 |
Martinez-Val, R. |
FLIGHT DYNAMICS OF THE FLYING WING |
ICAS 2008-5.8.3 |
Martins, A. L. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
Marulo, F. |
FE STUDY OF WINDSHIELD SUBJECTED TO HIGH SPEED BIRD IMPACT |
ICAS 2008-9.4.3 |
Marulo, F. |
PRACTICAL AEROELASTIC CALCULATIONS FOR LIGHT AIRPLANES |
ICAS2008-7.7 ST: |
Maruyama, D. |
AERODYNAMIC DESIGN OF THREE-DIMENSIONAL BIPLANE WINGS FOR LOW-WAVE DRAG SUPERSONIC FLIGHT |
ICAS 2008-2.4.4 |
Masahiro, K. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
Masarati, P. |
BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS |
ICAS 2008-9.10.4 |
Masarati, P. |
DEVELOPMENT AND VALIDATION OF AN INVESTIGATION TOOL FOR NONLINEAR AEROELASTIC ANALYSIS |
ICAS 2008-9.6.3 |
Masui, K. |
RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM - PART 2 FLIGHT EXPERIMENTS |
ICAS 2008-5.10.2 |
Matejka, M. |
SEPARATION CONTROL BY SYNTHETIC JET ACTUATOR IN STRAIGHT BLADE CASCADE |
ICAS 2008-3.10.4 |
Matsuno, T. |
FOREBODY VORTEX CONTROL ON HIGH PERFORMANCE AIRCRAFT USING PWM-CONTROLLED PLASMA ACTUATORS |
ICAS 2008-3.3.4 |
Mattaboni, M. |
BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS |
ICAS 2008-9.10.4 |
Mattiazzo, G. |
FLY-BY-WIRE CONTROL OF A HELICOPTER: MULTIBODY MAIN ROTOR MODEL |
ICAS2008-5.11 ST: |
Mattos, W. S. |
APPLICATION OF A MODEL UPDATING METHOD TO AN AIRCRAFT LONGITUDINAL STABILITY AUGMENTATION SYSTEM |
ICAS2008-5.2 ST: |
Maurice, L. |
GOING GREEN – MITIGATING AVIATION’S NEW ENVIRONMENTAL DRIVERS |
ICAS 2008-4.7.2 |
Maurice, L. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
Mavris, D. |
A METHODOLOGICAL APPROACH FOR AIRPORT TECHNOLOGY EVALUATION AND SELECTION |
ICAS 2008-8.3.4 (AIAA 2008-8965) |
Mavris, D. |
AN APPROACH FOR MULTI-CRITERIA DECISION MAKING METHOD SELECTION AND DEVELOPMENT |
ICAS 2008-1.3.1 |
Mavris, D. |
FUNCTION BASED ARCHITECTURE DESIGN SPACE DEFINITION AND EXPLORATION |
ICAS 2008-1.9.3 (AIAA 2008-8928) |
Mavris, D. |
METHODOLOGY FOR AIRCRAFT SYSTEM ARCHITECTURE SIZING |
ICAS 2008-6.2.2 |
Mavris, D. |
PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES |
ICAS2008-6.6 ST (AIAA 2008-8973) |
Mavris, D. N. |
ADVANCED GENERAL AVIATION DESIGN WITH TRANSPORTATION ARCHITECTURE ANALYSIS |
ICAS 2008-1.9.4 (AIAA 2008-8929) |
Mavris, D. N. |
AN APPROACH FOR VERIFICATION AND VALIDATION OF THE ENVIRONMENTAL DESIGN SPACE |
ICAS2008-P8.4 (AIAA 2008-8875) |
Mavris, D. N. |
DEMAND-CENTRIC ANALYSIS OF THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-10.4.3 (AIAA 2008-8889) |
Mavris, D. N. |
PARAMETRIC SYSTEM EFFECTIVENESS ANALYSIS USING ARTIFICIAL NEURAL NETWORKS FOR BATTLE MANAGEMENT |
ICAS 2008-1.3.3 |
Mavris, D. N. |
THE ENVIRONMENTAL DESIGN SPACE |
ICAS 2008-4.7.3 |
Mayer, R. H. |
BENEFIT POTENTIAL OF CONTINUOUS CLIMB AND DESCENT OPERATIONS |
ICAS 2008-11.8.2 (AIAA 2008-8920) |
Mayer, R. H. |
IMPROVING TERMINAL OPERATIONS - BENEFITS OF RNAV DEPARTURE PROCEDURES AT DALLAS-FORT WORTH AND HARTSFIELD-JACKSON ATLANTA INTERNATIONAL AIRPORTS |
ICAS 2008-11.1.3 (AIAA 2008-8856) |
Mayo, J. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
Mazlum, E. |
A COMPARISON OF NUMERICAL RANS SIMULATIONS AND FLOW FIELD MEASUREMENTS OF AN OSCILLATING AIRFOIL FOR FLAPPING WING PROPULSION |
ICAS 2008-2.10.2 |
Mazzotta, D. |
METHODOLOGY OPTIMIZATION OF METAL CUTTING PROGRAMMING APPLIED TO AERONAUTICAL COMPONENTS |
ICAS 2008-6.10.5 |
McAlleenen, C. |
AEROSPACE PRODUCT COST MANAGEMENT AT THE EARLY CONCEPT OPERATIONS PHASE |
ICAS 2008-10.6.2 (AIAA 2008-8904) |
McClean, A. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
McCoy, P. |
DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS |
ICAS 2008-6.7.4 |
McNally, D. |
AUTOMATED SEPARATION ASSURANCE IN THE PRESENCE OF UNCERTAINTY |
ICAS 2008-8.11.1 |
McNichols, W. M. |
CAUSALITY ANALYSIS FOR AVIATION WEATHER HAZARDS |
ICAS 2008-10.7.1 (AIAA 2008-8914) |
McRoberts, R. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
Mead, R. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
Mébarki, Y. |
COMPUTATIONAL FLUID DYNAMICS AND EXPERIMENTAL INVESTIGATION OF AIRPLANE STALL DYNAMICS WITH WING CONTAMINATION |
ICAS 2008-3.5.2 |
Mébarki, Y. |
TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT |
ICAS 2008-2.9.2 |
Meier, C. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
Melby, P. |
BENEFIT POTENTIAL OF CONTINUOUS CLIMB AND DESCENT OPERATIONS |
ICAS 2008-11.8.2 (AIAA 2008-8920) |
Melia, J. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
Mellert, V. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
Mello Jr., A. W. S. |
SIMPLIFYING MSD MODELING BY USING CONTINUING DAMAGE ASSUMPTION AND PARAMETRIC STUDY: THE ROLE OF RIVET SQUEEZE FORCE |
ICAS 2008-9.8.1 |
Mendez, J. |
FATIGUE DESIGN OF METALLIC COMPONENTS CONTAINING SURFACE OR INTERNAL DEFECTS |
ICAS 2008-7.4.3 |
Mendez, J. |
SIZE OPTIMIZATION OF AIRCRAFT STRUCTURES |
ICAS2008-7.11 ST: |
Menéndez, X. P. |
CAPACITY MODELLING FOR FUTURE AERONAUTICAL SAFETY COMMUNICATIONS OVER WIDE AREAS |
ICAS 2008-8.8.2 (AIAA 2008-8952) |
Menon, P. K. |
MODEL-BASED AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.1 (AIAA 2008-8907) |
Menon, P. K. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
Menon, P. K. |
RAPID PREDICTION OF AIR TRAFFIC FOR TRAJECTORY BASED OPERATIONS |
ICAS2008-11.6 ST (AIAA 2008-8902) |
Menon, P. K. |
TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.1.1 (AIAA 2008-8854) |
Merazzi, S. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
Mercer, J. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
Mercer, J. |
HUMAN-IN-THE-LOOP EVALUATION OF GROUND-BASED AUTOMATED SEPARATION ASSURANCE FOR NEXTGEN |
ICAS 2008-11.4.5 (AIAA 2008-8885) |
Mermet-Guyennet, M. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
Meuret, R. |
HIGH EFFICIENCY, HIGH RELIABILITY 2 KW INVERTER FOR AERONAUTICAL APPLICATION |
ICAS 2008-6.1.3 |
Meuret, R. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
Meussen, M. |
LONG TERM AIRCRAFT PROJECT AND TECHNOLOGY EVALUATION UNDER THE UNCERTAINTY OF FUTURE SCENARIOS |
ICAS 2008-1.3.4 |
Micol, A. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
Miller, M. E. |
NETWORK ENABLED OPERATIONS ENHANCES AVIATION EFFICIENCY |
ICAS 2008-8.8.1 (AIAA 2008-8951) |
Min, B. M. |
PERFORMANCE EVALUATION AND HILS TEST OF CONTROL ALLOCATION METHODS FOR RECONFIGURATION CONTROL |
ICAS 2008-5.10.3 |
Miquel, T. |
MODIFIED BEZIER CURVE FOR 4D REFERENCE TRAJECTORY DEFINITION UNDER FLIGHT PROFILE CONSTRAINT |
ICAS 2008-11.6.3 (AIAA 2008-8900) |
Miranda, G. |
3D OBSTACLE AVOIDANCE STRATEGIES FOR UAS (UNINHABITED AERIAL SYSTEMS) MISSION PLANNING AND RE-PLANNING |
ICAS 2008-5.6.1 (AIAA 2008-8962) |
Mirzoyan, A. A. |
STUDIES ON MDO OF ENGINE DESIGN PARAMETERS WITH MISSION, NOISE & EMISSION CRITERIA AT SSBJ ENGINE CONCEPTUAL DESIGN |
ICAS 2008-4.2.3 |
Mistry, S. |
NOVEL DESIGN CONCEPTS FOR AIRCRAFT WITH REDUCED NOISE AND GLOBAL WARMING CHARACTERISTICS |
ICAS 2008-4.10.4 |
Moccia, A. |
DEVELOPMENT AND TEST OF AN INTEGRATED SENSOR SYSTEM FOR AUTONOMOUS COLLISION AVOIDANCE |
ICAS2008-P6.12 |
Mohamed, K. |
KRYLOV RECYCLING TECHNIQUES FOR UNSTEADY SIMULATION OF TURBULENT AERODYNAMIC FLOWS |
ICAS2008-2.1 ST: |
Möhlenbrink, C. |
AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION |
ICAS 2008-8.3.1 |
Moir, S. |
AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS |
ICAS 2008-3.11.3 |
Monclar, P. |
LATEST DEVELOPMENTS IN ELECTRIAL LANDING SYSTEMS |
ICAS 2008-6.5.3 |
Mondali, M. |
AN ANALYTICAL MODEL FOR PREDICTION OF THE STEADY STATE CREEP DEFORMATIONS AND STRESSES OF SHORT FIBER COMPOSITES |
ICAS 2008-9.8.3 |
Montgomery, J. |
ENVIRONMENTALLY PROGRESSIVE AIRPLANES THROUGH AN INTEGRATED DESIGN FOR INTERIOR NOISE |
ICAS 2008-4.9.1 INVITED |
Montoya, J. |
AN OPTIMIZATION MODEL FOR REDUCING AIRCRAFT TAXI TIMES AT THE DALLAS-FORT WORTH INTERNATIONAL AIRPORT |
ICAS 2008-8.6.1 |
Moore, D. P. |
147 THE LOW DOWN – DIGITAL TERRAIN DATA FOR AUTOMATIC GROUND COLLISION AVOIDANCE |
ICAS2008-P6.10 |
Moorhouse, D. |
NUMERICAL STUDY OF ENERGY UTILIZATION IN NOZZLE/PLUME FLOW-FIELDS OF HIGH-SPEED AIR-BREATHING VEHICLES |
ICAS 2008-4.3.3 |
Mora-Camino, F. |
MODIFIED BEZIER CURVE FOR 4D REFERENCE TRAJECTORY DEFINITION UNDER FLIGHT PROFILE CONSTRAINT |
ICAS 2008-11.6.3 (AIAA 2008-8900) |
Morgado Belo, E. M. |
INFLUENCES INVESTIGATION OF NUMERICAL PARAMETERS AND MESHING ON THE AEROELASTIC RESPONSE |
ICAS2008- P3.4 |
Morgado Belo, E. M. |
NUMERICAL DEVELOPMENT OF A FLUTTER ACTIVE CONTROL SYSTEM BASED ON PRESSURE FEEDBACK. |
ICAS2008-P3.3 |
Mori, R. |
NEURAL NETWORK ANALYSIS OF PILOT MANEUVER DURING LANDING PHASE |
ICAS 2008-5.4.4 |
Morris, A. M. |
TOWARDS AERODYNAMIC OPTIMISATION OF AN AEROELASTIC WING USING DOMAIN ELEMENT PARAMETERISATION |
ICAS 2008-2.8.1 |
Morrow, C. |
SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT |
ICAS 2008-11.2.2 (AIAA 2008-8858) |
Motamedian, H. R. |
MICROMECHANICAL FEM MODELING OF THERMAL STRESSES IN FUNCTIONALLY GRADED MATERIALS |
ICAS 2008-7.2.4 |
Motogoe, S. |
ESTIMATION OF THE INFLUENCE OF PROFILE ERROR ON AERODYNAMIC PERFORMANCE FOR LOW-REYNOLDS-NUMBER AIRFOILS |
ICAS2008-3.7 ST: |
Muehlhausen, T. |
THE USE OF MODELS FOR ATM VALIDATION: FROM AIRPORT EXTENSION PROGRAMS TO THE AIR TRANSPORT SYSTEM OF THE FUTURE |
ICAS2008-8.9 ST: |
Mueller, B. E. |
METHODOLOGY FOR THERMALLY INDUCED LOADING IN STRUCTURAL ANALYSIS ON THE F-35 LIGHTNING II |
ICAS 2008-7.11.1 |
Mueller, E. |
FLIGHT DECK PROCEDURAL GUIDELINES FOR DATALINK TRAJECTORY NEGOTIATIONS |
ICAS 2008-11.6.4 (AIAA 2008-8901) |
Muffo, D. |
COMPRESSIBLE FLUID-FLOW ALE FORMULATION ON CHANGING TOPOLOGY MESHES FOR AEROELASTIC SIMULATIONS |
ICAS2008-2.10 ST: |
Mulder, M. |
FEASIBILITY ANALYSIS OF ACHIEVING A STABILIZED APPROACH |
ICAS 2008-5.4.2 |
Mulder, T. J. |
ON THE REDUCTION OF NOX-EMISSION LEVELS BY PERFORMING LOW NOX FLIGHTS |
ICAS2008-4.7 ST: |
Mullan, M. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
Mulyanto, T. |
643 DEVELOPMENT OF A COAXIAL ROTOR MAV FOR INDOOR APPLICATION |
ICAS2008-P1.9 |
Mundra, A. D. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
Murayama, M. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
Murayama, M. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
Murdoch, J. L. |
OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM |
ICAS 2008-11.6.1 (AIAA 2008-8898) |
Murdoch, J. L. |
PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY |
ICAS 2008-10.5.2 (AIAA 2008-8896) |
Murphy, D. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
Musaj, M. |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE AERODYNAMICS OF UNCONVENTIONAL W-LEADING EDGE REVERSED DELTA WING IN GROUND EFFECT |
ICAS 2008-3.5.3 |
Myerscough, K. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
Nadarajah, S. |
KRYLOV RECYCLING TECHNIQUES FOR UNSTEADY SIMULATION OF TURBULENT AERODYNAMIC FLOWS |
ICAS2008-2.1 ST: |
Nadot, Y. |
FATIGUE DESIGN OF METALLIC COMPONENTS CONTAINING SURFACE OR INTERNAL DEFECTS |
ICAS 2008-7.4.3 |
Nadot-Martin, C. |
A MULTI-SCALE “MORPHOLOGICAL APPROACH” FOR MODELING THE NON LINEAR BEHAVIOR OF PROPELLANT-LIKE MATERIALS |
ICAS 2008-7.1.3 |
Nag, M. |
TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.1.1 (AIAA 2008-8854) |
Nagai, H. |
EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE |
ICAS 2008-3.7.5 |
Nagai, H. |
MEASUREMENT OF UNSTEADY AERODYNAMIC FORCES OF 3D FLAPPING WING IN HOVERING TO FORWARD FLIGHT |
ICAS 2008-3.4.3 |
Nagai, K. |
AERODYNAMIC DESIGN AND ITS VALIDATION OF AN OPEN-TYPE ENGINE RUN-UP FACILITY |
ICAS 2008-4.5.3 |
Nagaoka, S. |
A MODEL FOR ESTIMATING THE LATERAL OVERLAP PROBABILITY OF AIRCRAFT WITH RNP ALERTING CAPABILITY IN PARALLEL RNAV ROUTES |
ICAS 2008-9.7.5 |
Nagaoka, S. |
ANALYSIS OF GAPS BETWEEN THE PREDICTIVE AND THE ADAPTIVE COMPONENT IN ATM |
ICAS 2008-11.10.2 (AIAA 2008-8941) |
Nagasaka, N. |
AUTONOMOUS AERIAL OBSERVATION SYSTEM FOR DISASTER RESPONSE USING ELECTRIC DUCTED FAN MAVS |
ICAS 2008-1.4.5 |
Nagel, B. |
ACTIVE AND PASSIVE STRUCTURAL MEASURES FOR AEROELASTIC WINGLET DESIGN |
ICAS 2008-7.10.1 |
Nagy, A. |
INVESTIGATION ON THE EFFECT OF HYDRODYNAMIC MEMS ON AIRFOIL |
ICAS2008-3.10 ST: |
Nakahashi, K. |
MULTI-DISCIPLINARY DESIGN EXPLORATION FOR WINGLET |
ICAS 2008-1.1.3 |
Nakakita, K. |
TRANSONIC FLUTTER WIND TUNNEL TESTS OF CONVENTIONAL TWIN-ENGINE TRANSPORT SEMISPAN MODEL |
ICAS 2008-9.6.2 |
Nakamichi, J. |
TRANSONIC FLUTTER WIND TUNNEL TESTS OF CONVENTIONAL TWIN-ENGINE TRANSPORT SEMISPAN MODEL |
ICAS 2008-9.6.2 |
Nangia, R. K. |
ACHIEVING HIGHLY EFFICIENT CIVIL AVIATION - WHY & HOW WITH AIR-TO-AIR REFUELLING, REVIEW & NEW DEVELOPMENTS |
ICAS 2008-4.10.1 |
Nangia, R. K. |
SUPERSONIC AIRCRAFT FORMATION FLYING TO INCREASE FLIGHT EFFICIENCY |
ICAS 2008-1.10.2 |
Nardin, L. |
AERODYNAMIC OPTIMIZATION OF AIRCRAFT CONFIGURATIONS WITH MULTIDISZIPLINARY ASPECTS |
ICAS 2008-2.11.3 |
Narkiewicz, J. P. |
NONLINEAR MODEL FOLLOWING RECONFIGURABLE FLIGHT CONTROL SYSTEM |
ICAS 2008-5.10.4 |
Naruoka, M. |
ATTITUDE ACCURACY IMPROVEMENT OF ULTRA LOW-GRADE MEMS INS USING ALIGNMENT OF GPS ANNTENA |
ICAS2008-P6.11 |
Natan, B. |
PULSATING COMBUSTION OF AN ORGANIC GEL-FUEL DROPLET AND ITS INFLUENCE ON THE THERMAL FIELD OF A SPRAY DIFFUSION FLAME |
ICAS 2008-4.1.2 |
Navazi, H. M. |
SCALED DOWN MODELS FOR FREE VIBRATION ANALYSIS OF ORTHOGONALLY STIFFENED CYLINDRICAL SHELLS USING SIMILITUDE THEORY |
ICAS 2008-7.7.5 |
Négrier, J. |
DESIGN OF A SMALL SUPERSONIC TRANSPORT AIRCRAFT WITH HIGH ENVIRONMENTAL CONSTRAINTS |
ICAS 2008-1.10.1 INVITED |
Nejjari, F. |
HIERARCHICAL AND SENSITIVITY ANALYSIS FOR NOISE ABATEMENT DEPARTURE PROCEDURES |
ICAS 2008-11.3.3 (AIAA 2008-8867) |
Nelson, R. C. |
FOREBODY VORTEX CONTROL ON HIGH PERFORMANCE AIRCRAFT USING PWM-CONTROLLED PLASMA ACTUATORS |
ICAS 2008-3.3.4 |
Nesterenko, B. G. |
ESTIMATION OF CRACK TURN PHENOMENON |
ICAS 2008-7.6.3 |
Nesterenko, G. I. |
ESTIMATION OF CRACK TURN PHENOMENON |
ICAS 2008-7.6.3 |
Ng, A. |
SUITABILITY OF DIFFERENT CRACK GROWTH MODELS FOR ANALYSING MULTI-SITE DAMAGE IN AIRCRAFT STRUCTURAL CONFIGURATIONS |
ICAS2008-7.6 ST: |
Nguyen Van, T. |
SYSTEM INFRASTRUCTURE FOR INTEGRATED AND COLLABORATIVE PRODUCT DEVELOPMENT IN THE AERONAUTIC INDUSTRY |
ICAS 2008-6.10.2 |
Nibourg, J. M. |
ENVIRONMENT-AWARE RUNWAY ALLOCATION ADVICE SYSTEM |
ICAS 2008-4.11.2 |
Nicolosi, F. |
DESIGN AND AERODYNAMIC ANALYSIS OF A LIGHT TWIN ENGINE PROPELLER AIRCRAFT |
ICAS 2008-1.2.2 |
Nicolosi, F. |
SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION |
ICAS 2008-2.7.3 |
Niedringhaus, W. P. |
USING AIRSPACEANALYZER TO EFFICIENTLY PROVIDE SPACING FOR AIRCRAFT ACROSS MULTIPLE SECTORS |
ICAS 2008-11.2.4 (AIAA 2008-8860 ) |
Niesner, R. |
NUMERICAL ANALYSIS OF THIN-WALLED STRUCTURES IN HYPERSONIC FLOW REGIME |
ICAS 2008-3.6.1 |
Nigmatullin, R. Z. |
UNSTEADY CFD MODELING OF WHOLE GAS TURBINE ENGINE FLOW PASSAGE WITH APPLICATIONS |
ICAS2008-4.4 ST: |
Nitsche, W. |
A WALL SHEAR STRESS MEASUREMENT TECHNIQUE USING THE THERMAL WAKES OF SMALL HEATED SPOTS |
ICAS 2008-3.7.1 |
Nitsche, W. |
ACTIVE CANCELLATION OF TOLLMIEN-SCHLICHTING INSTABILITIES UP TO M = 0.40 |
ICAS 2008-3.10.2 |
Nitsche, W. |
ACTIVE SEPARATION CONTROL ON A SLATLESS 2D HIGH-LIFT WING SECTION |
ICAS 2008-3.11.2 |
Nitsche, W. |
IN-FLIGHT EXPERIMENTS FOR DELAYING LAMINAR-TURBULENT TRANSITION ON A LAMINAR WING GLOVE |
ICAS 2008-3.7.3 |
Noda, F. |
CBAQ: DEVELOPMENT OF CRM BEHAVIOR ANALYSIS METHOD FOR MISSION FLIGHT CREW TRAINING |
ICAS 2008-9.2.1 |
Noguchi, M. |
NUMERICAL STUDY OF A PITOT PROBE WITH FIVE-HOLE PYRAMIDAL HEAD FOR SUPERSONIC FLIGHT TEST |
ICAS 2008-3.2.4 |
Noonan, K. |
NATSIM: A SYSTEMS DYNAMICS MODEL OF NORTH ATLANTIC AIR TRAFFIC |
ICAS 2008-9.11.3 (AIAA 2008-8912) |
Noonan, K. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
Noordman, B. A. T. |
OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION |
ICAS 2008-2.11.2 |
Nozicka, J. |
SEPARATION CONTROL BY SYNTHETIC JET ACTUATOR IN STRAIGHT BLADE CASCADE |
ICAS 2008-3.10.4 |
Obayashi, S. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
Ochieng, W. |
SATELLITE-BASED NAVIGATION ARCHITECTURE STUDY FOR AIRCRAFT CATEGORY III LANDINGS |
ICAS 2008-6.4.4 |
Ogawa, T. |
EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE |
ICAS 2008-3.7.5 |
Ogawa, T. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
Oheimb, D. von |
SECURITY ARCHITECTURE AND FORMAL ANALYSIS OF AN AIRPLANE SOFTWARE DISTRIBUTION SYSTEM |
ICAS 2008-9.1.1 |
Oliveira, G. L. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
Oliveira, J. M. G. S. |
ON THE EFFECTS ON NOISE OF GROUND REFLECTION AND ATMOSPHERIC ATTENUATION ON THE NOISE OF HELICOPTERS |
ICAS 2008-3.9.4 |
Olsen, R. F. |
MODELING OF ACOUSTICALLY TREATED NACELLE LIP TRANSPIRATION FLOW ANTI-ICING SYSTEM |
ICAS 2008-6.4.3 |
Olsson, P. -M. |
ROUTE PLANNING FOR RELAY UAV |
ICAS 2008-5.6.2 |
Ölvander, J. |
A QUANTIFIED RELATIONSHIP MATRIX AIDED BY PROBABILISTIC DESIGN AND OPTIMIZATION |
ICAS 2008-6.2.1 |
Omar, Z. |
GENETIC FUZZY CONTROL FOR AUTONOMOUS DUCTED-FAN VTOL UAV |
ICAS 2008-5.9.3 |
Ommi, F. |
EXPERIMENTAL INVESTIGATION OF SPRAY CHARACTERISTICS OF DOUBLE-BASE SWIRL INJECTOR |
ICAS2008-4.1 ST: |
Onorato, M. |
INVESTIGATION OF THE FLOW IN A RECTANGULAR CAVITY USING TOMOGRAPHIC AND TIME-RESOLVED PIV |
ICAS 2008-3.2.2 |
Onorato, M. |
THE EFFECTS OF WALL ROUGHNESS ON THE TURBULENT BOUNDARY LAYER |
ICAS 2008-3.8.1 |
Oppelstrup, J. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
Orchard, D. M. |
THE APPLICATION OF SEMI-EMPIRICAL STORE RELEASE SIMULATION FOR THE OPTIMIZATION OF GRID SURVEY WIND TUNNEL TESTING |
ICAS 2008-3.1.3 |
Orieux, S. |
AUTOMATED GENERATION, SELECTION AND EVALUATION OF ARCHITECTURES FOR ELECTROMECHANICAL ACTUATORS |
ICAS 2008-6.6.1 |
Orifici, A. C. |
THE DESIGN OF POSTBUCKLING COMPOSITE AEROSPACE STRUCTURES ACCOUNTING FOR DAMAGE INITIATION AND GROWTH |
ICAS 2008-7.3.2 |
Ortiz, D. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
Ostwald, P. |
AIRSPACE SECURITY MEASURES EMPLOYED FOR THE UN GENERAL ASSEMBLY MEETING: ANALYSIS AND IMPACT |
ICAS 2008-11.5.1 (AIAA 2008-8892) |
Ostwald, P. |
INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.10.1 (AIAA 2008-8940) |
Owen, B. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Oyama, S. |
EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE |
ICAS 2008-3.7.5 |
Ozaki, S. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
Oztekin, A. |
HAZARD, SAFETY RISK AND UNCERTAINTY MODELING OF THE INTEGRATION OF UNMANNED AIRCRAFT SYSTEMS INTO THE NATIONAL AIRSPACE |
ICAS 2008-9.7.2 |
Paglione, P. |
A PROCEDURE TO DESIGN AIRCRAFT FLIGHT CONTROL LAWS TAKING INTO ACCOUNT ROBUSTNESS USING THE VARIABLE STRUCTURE CONTROL |
ICAS2008-5.4 ST: |
Paielli, R. A. |
TACTICAL CONFLICT RESOLUTION USING VERTICAL MANEUVERS IN ENROUTE AIRSPACE |
ICAS2008-11.4 ST (AIAA 2008-8886) |
Pak, C. -G. |
STRUCTURAL MODEL TUNING CAPABILITY IN AN OBJECT-ORIENTED MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL |
ICAS 2008-9.5.1 |
Pak, C.-G. |
MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL DEVELOPMENT USING GENETIC ALGORITHM |
ICAS 2008-1.1.1 |
Palaniappan, K. |
TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.1.1 (AIAA 2008-8854) |
Palmer, E. |
CONTROLLER SUPPORT FOR MANAGING HIGH-EFFICIENCY ARRIVALS IN DENSE TRAFFIC ENVIRONMENTS |
ICAS 2008-11.10.4 (AIAA 2008-8943) |
Palmer, M. E. |
SUPERSONIC AIRCRAFT FORMATION FLYING TO INCREASE FLIGHT EFFICIENCY |
ICAS 2008-1.10.2 |
Pant, R. |
INCLUSION OF ENGINE RELATED PARAMETERS IN CONCEPTUAL DESIGN OF MORPHING AIRCRAFT |
ICAS 2008-1.6.4 |
Pant, R. S. |
DESIGN, FABRICATION AND OPERATION OF REMOTELY CONTROLLED AIRSHIPS IN INDIA |
ICAS 2008-10.1.3 (AIAA 2008-8853) |
Pant, R. S. |
LOW COST TRANS-RIVER AERIAL-FERRY USING A NOVEL LTA SYSTEM |
ICAS 2008-10.1.2 (AIAA 2008-8851) |
Paraschivoiu, M. |
KRYLOV RECYCLING TECHNIQUES FOR UNSTEADY SIMULATION OF TURBULENT AERODYNAMIC FLOWS |
ICAS2008-2.1 ST: |
Parekh, D. |
DESIGN OF A NOVEL INTELLIGENT DATA MANAGEMENT TOOL FOR HEALTH AND USAGE MONITORING SYSTEMS – DESIGN REQUIREMENTS |
ICAS2008-6.1 ST: |
Parezanovic, V. |
ON AIRCRAFT PERFORMANCE IMPROVEMENT BY USING WINGLETS |
ICAS 2008-2.8.3 |
Park, H. -U. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
Pascale, L. |
DESIGN AND AERODYNAMIC ANALYSIS OF A LIGHT TWIN ENGINE PROPELLER AIRCRAFT |
ICAS 2008-1.2.2 |
Pastorelli, S. |
FLY-BY-WIRE CONTROL OF A HELICOPTER: MULTIBODY MAIN ROTOR MODEL |
ICAS2008-5.11 ST: |
Patek, Z. |
PERFORMANCE DEGRADATION OF A SIMULATED ICE CONTAMINATED AIRFOIL BY SUPER-COOLED DROPLETS |
ICAS 2008-3.7.2 |
Pátek, Z. |
WIND TUNNEL AND COMPUTIONAL INVESTIGATION OF SIMULATED CONTAMINATION ON AIRFOIL |
ICAS2008-P2.11 |
Patel, C. K. |
THEORETICAL AND EXPERIMENTAL INVESTIGATION OF ENERGY EXTRACTION FROM ATMOSPHERIC TURBULENCE |
ICAS2008-1.5 ST: |
Pätzold, A. |
IN-FLIGHT EXPERIMENTS FOR DELAYING LAMINAR-TURBULENT TRANSITION ON A LAMINAR WING GLOVE |
ICAS 2008-3.7.3 |
Paul, D. |
FLIGHT VEHICLE COMPOSITE STRUCTURES |
ICAS 2008-7.9.1 (AIAA 2008-8976 ) |
Paull, G. |
OPERATIONAL ASSESSMENT OF THE INTEGRATED TERMINAL WEATHER SYSTEM (ITWS) USING DIRECT MEASUREMENT |
ICAS 2008-10.7.5 (AIAA 2008-8918) |
Pe, T. |
MULTIVARIABLE CONTROLLER DESIGN FOR A TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WITH TWO PRIMARY LOAD PATHS |
ICAS 2008-6.4.2 |
Pechloff, A. |
SMALL DISTURBANCE NAVIER-STOKES COMPUTATIONS FOR LOW ASPECT RATIO WING PITCHING OSCILLATIONS |
ICAS 2008-2.10.3 |
Peigin, S. |
EFFICIENT APPROACH FOR MULTIPOINT AERODYNAMIC WING DESIGN OF BUSINESS JET AIRCRAFT |
ICAS 2008-2.11.1 |
Peigin, S. |
HYBRIDIZATION OF HETEROGENEOUS 3D CFD DISCRETIZATIONS VIA DIRECT FLUX OPTIMIZATION |
ICAS2008-2.3 ST: |
Peltzer, I. |
ACTIVE SEPARATION CONTROL ON A SLATLESS 2D HIGH-LIFT WING SECTION |
ICAS 2008-3.11.2 |
Peltzer, I. |
IN-FLIGHT EXPERIMENTS FOR DELAYING LAMINAR-TURBULENT TRANSITION ON A LAMINAR WING GLOVE |
ICAS 2008-3.7.3 |
Peraire, J. |
COMPUTATIONAL INVESTIGATION AND DESIGN OF COMPLIANT MEMBRANE WINGS FOR BIOLOGICALLY INSPIRED FLIGHT VEHICLES |
ICAS 2008-2.10.1 |
Perebatov, V. |
THEORETICAL APPROACH TO DIRECTIONAL CONTROL SENSITIVITY SELECTION |
ICAS 2008-5.4.1 INVITED |
Pereira, G. A. S. |
DEVELOPMENT OF A SMALL UNMANNED AIR VEHICLE WITH MINIMUM SENSORS PHILOSOPHY |
ICAS2008-1.4 ST: |
Pereira, N. C. |
APPLICATION OF A MODEL UPDATING METHOD TO AN AIRCRAFT LONGITUDINAL STABILITY AUGMENTATION SYSTEM |
ICAS2008-5.2 ST: |
Perez, E. |
AIRPLANE DESIGN: A MUST IN AERONAUTICAL ENGINEERING EDUCATION |
ICAS2008-P1.6 |
Persiani, F. |
3D OBSTACLE AVOIDANCE STRATEGIES FOR UAS (UNINHABITED AERIAL SYSTEMS) MISSION PLANNING AND RE-PLANNING |
ICAS 2008-5.6.1 (AIAA 2008-8962) |
Persiani, F. |
A NEW AIRCRAFT CONCEPT: THE COMBAT MALE |
ICAS 2008-1.4.4 |
Persiani, F. |
DESIGN AND DEVELOPMENT OF AN ATC DISTRIBUTED TRAINING SYSTEM |
ICAS2008-P8.2 (AIAA 2008-8873) |
Persiani, F. |
DESIGN AND EVALUATION OF A 4D INTERFACE FOR ATC |
ICAS 2008-9.10.3 |
Persson, I. |
TRANSONIC STORE SEPARATION STUDIES ON THE SAAB GRIPEN AIRCRAFT USING COMPUTATIONAL AERODYNAMICS |
ICAS 2008-2.9.1 |
Pesak, M. |
OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING - EXPERIMENTAL VERIFICATION |
ICAS 2008-9.5.2 |
Pezzella, G. |
ANALYSIS OF THERMOCHEMICAL MODELING AND SURFACE CATALYTICITY IN SPACE VEHICLES REENTRY |
ICAS 2008-3.6.2 |
Pfaender, H. |
A METHOD FOR ASSESSING THE ENVIRONMENTAL BENEFIT OF FUTURE AVIATION TECHNOLOGIES |
ICAS2008-P10.2 |
Pfeiffer, U. |
IMPACT RESISTANCE, DAMAGE TOLERANCE AND NON-DESTRUCTIVE DAMAGE DETECTION FOR SANDWICH STRUCTURES: ANALYSIS AND TESTING |
ICAS2008-7.5 ST: |
Phan, L. |
PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES |
ICAS2008-6.6 ST (AIAA 2008-8973) |
Phleps, P. |
IMPACT OF ESTOL CAPABILITY ON RUNWAY CAPACITY - AN ANALYTICAL APPROACH |
ICAS 2008-11.9.4 (AIAA 2008-8933) |
Piekert, F. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
Pierce, R. S. |
COMPARING SITUATION AWARENESS MEASUREMENT TECHNIQUES IN A LOW FIDELITY AIR TRAFFIC CONTROL SIMULATION |
ICAS 2008-9.7.4 |
Pinon, O. |
A METHODOLOGICAL APPROACH FOR AIRPORT TECHNOLOGY EVALUATION AND SELECTION |
ICAS 2008-8.3.4 (AIAA 2008-8965) |
Pires, M. |
TURBULENCE MODELING S AND APPLICATIONS TO AEROSPIKE PLUG NOZZLE |
ICAS 2008-4.1.3 |
Pistek, A. |
OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING - EXPERIMENTAL VERIFICATION |
ICAS 2008-9.5.2 |
Pittofrati, M. |
SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT |
ICAS 2008-7.9.2 |
Pizzolo, A. |
TRAJECTORY TRACKING FOR A NON - CONVENTIONAL UAV |
ICAS2008-P5.3 |
Plágaro, L. |
AERODYNAMIC OPTIMIZATION OF A BLENDED WING BODY |
ICAS2008-2.11 ST: |
Platzer, M. F. |
FLAPPING-WING TECHNOLOGY: THE POTENTIAL FOR AIR VEHICLE PROPULSION AND AIRBORNE POWER GENERATION |
ICAS 2008-1.5.1 |
Plegas, P. |
VIRTUAL ENTERPRISE COLLABORATION - BREAKTHROUGH TECHNOLOGIES PROVIDED BY VIVACE |
ICAS 2008-8.10.4 INVITED |
Ploetner, K. O. |
INVESTIGATION OF LONG-HAUL FLIGHT ATTRIBUTES INFLUENCING PASSENGER'S BOOKING DECISION USING SP DATA |
ICAS 2008-6.3.1 |
Pointon, J. M. |
THERMAL MANAGEMENT OF ELECTROMECHANICAL ACTUATION ON AN ALL-ELECTRIC AIRCRAFT |
ICAS 2008-6.6.2 |
Poovendran, R. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
Poovendran, R. |
SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-9.1.3 |
Popelka, L. |
SEPARATION CONTROL BY SYNTHETIC JET ACTUATOR IN STRAIGHT BLADE CASCADE |
ICAS 2008-3.10.4 |
Poppe, M. |
TOWARDS SESAR PERFORMANCE TARGETS - THE SUPER-HIGHWAY APPROACH |
ICAS 2008-10.10.1 (AIAA 2008-8935) |
Porter, D. J. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
Post, J. |
NATSIM: A SYSTEMS DYNAMICS MODEL OF NORTH ATLANTIC AIR TRAFFIC |
ICAS 2008-9.11.3 (AIAA 2008-8912) |
Post, J. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
Post, M. |
FLIGHT EVALUATION OF A COMPACT AIRBORNE TRACE GAS ANALYSIS SENSOR PROOF-OF-CONCEPT |
ICAS2008-P6.4 |
Prananta, B. B. |
EFFICIENT AEROELASTIC SIMULATION IN A PARAMETRIC PROCEDURE FOR FATIGUE ANALYSIS |
ICAS 2008-7.7.1 |
Prats, X. |
HIERARCHICAL AND SENSITIVITY ANALYSIS FOR NOISE ABATEMENT DEPARTURE PROCEDURES |
ICAS 2008-11.3.3 (AIAA 2008-8867) |
Pratt, D. |
FLIGHT VEHICLE COMPOSITE STRUCTURES |
ICAS 2008-7.9.1 (AIAA 2008-8976 ) |
Preatoni, M. L. |
FLIGHT MECHANICS SIMULATOR FOR ROTORCRAFT DEVELOPMENT |
ICAS2008-P5.4 |
Prete, J. |
CAUSALITY ANALYSIS FOR AVIATION WEATHER HAZARDS |
ICAS 2008-10.7.1 (AIAA 2008-8914) |
Prete, J. |
ON-DEMAND SPECIAL USE AIRSPACE |
ICAS 2008-10.10.4 (AIAA 2008-8938) |
Prete, J. |
PRINCIPLES OF AIRSPACE TUBE DESIGN FOR DYNAMIC AIRSPACE CONFIGURATION |
ICAS 2008-10.10.5 (AIAA 2008-8939) |
Prevot, T. |
HUMAN-IN-THE-LOOP EVALUATION OF GROUND-BASED AUTOMATED SEPARATION ASSURANCE FOR NEXTGEN |
ICAS 2008-11.4.5 (AIAA 2008-8885) |
Prince, S. A. |
AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS |
ICAS 2008-3.11.3 |
Prince, S. A. |
AN EXPERIMENTAL AND COMPUTATIONAL COMPARISON OF THE LOW SPEED AERODYNAMICS OF SQUARE AND CIRCULAR SECTIONED BODIES |
ICAS2008-3.5 ST: |
Prince, S. A. |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE AERODYNAMICS OF UNCONVENTIONAL W-LEADING EDGE REVERSED DELTA WING IN GROUND EFFECT |
ICAS 2008-3.5.3 |
Prince, S. A. |
VORTEX SHEDDING FROM A ROTATING CIRCULAR CYLINDER AT MODERATE SUB-CRITICAL REYNOLDS NUMBERS AND HIGH VELOCITY RATIO |
ICAS 2008-3.10.5 |
Prisell, E. |
A STUDY OF AN USER AND ENVIRONMENTAL FRIENDLY STORED ENERGY BASED EPU/APU-SYSTEM FOR MILITARY AEROSPACE APPLICATIONS |
ICAS 2008-6.4.5 |
Pronk, F. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
Przytula, K. W. |
HEALTH MONITORING FOR COMMERCIAL AIRCRAFT SYSTEMS |
ICAS 2008-6.1.2 |
Puig, V. |
HIERARCHICAL AND SENSITIVITY ANALYSIS FOR NOISE ABATEMENT DEPARTURE PROCEDURES |
ICAS 2008-11.3.3 (AIAA 2008-8867) |
Qiao, Z. D. |
LIFT PREDICTION OF MULTI-ELEMENT AIRFOIL USING DES AND RANS |
ICAS2008-P2.5 |
Qiao, Z. D. |
RESEARCH ON MONITORING AND CONTROL SYSTEM BASED PLC IN THE NF-6 WIND TUNNEL |
ICAS2008-P2.10 |
Qiao, Z. H. D. |
AERODYNAMIC SHAPE OPTIMIZATION OF TRANSONIC AEROELASTIC WING BASED ON CONTROL THEORY |
ICAS2008-9.6 ST: |
Qiao, Z.D. |
TRANSONIC FLUTTER ANALYSIS OF AN AIRFOIL WITH APPROXIMATE BOUNDARY METHOD |
ICAS 2008-7.10.5 |
Quagliotti, F. |
TRAJECTORY OPTIMISATION FOR AUTONOMOUS VEHICLES: A MINIUAV APPLICATION |
ICAS 2008-5.6.3 |
Quaranta, G. |
BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS |
ICAS 2008-9.10.4 |
Quaranta, G. |
COMPRESSIBLE FLUID-FLOW ALE FORMULATION ON CHANGING TOPOLOGY MESHES FOR AEROELASTIC SIMULATIONS |
ICAS2008-2.10 ST: |
Quest, J. |
DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS |
ICAS 2008-3.2.1 |
Quevedo, J. |
HIERARCHICAL AND SENSITIVITY ANALYSIS FOR NOISE ABATEMENT DEPARTURE PROCEDURES |
ICAS 2008-11.3.3 (AIAA 2008-8867) |
Rachami, J. |
SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT |
ICAS 2008-11.2.2 (AIAA 2008-8858) |
Radespiel, R. |
A COMPARISON OF NUMERICAL RANS SIMULATIONS AND FLOW FIELD MEASUREMENTS OF AN OSCILLATING AIRFOIL FOR FLAPPING WING PROPULSION |
ICAS 2008-2.10.2 |
Ragazzi, A. |
FLIGHT MECHANICS SIMULATOR FOR ROTORCRAFT DEVELOPMENT |
ICAS2008-P5.4 |
Raghunathan, S. |
EXCRESCENCES EFFECTS IN AERODYNAMICS |
ICAS2008-3.8 ST: |
Raghunathan, S. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
Raina, A. A. |
DESIGN, FABRICATION AND OPERATION OF REMOTELY CONTROLLED AIRSHIPS IN INDIA |
ICAS 2008-10.1.3 (AIAA 2008-8853) |
Raina, A. A. |
LOW COST TRANS-RIVER AERIAL-FERRY USING A NOVEL LTA SYSTEM |
ICAS 2008-10.1.2 (AIAA 2008-8851) |
Ramesh, A. |
ADVANCED METHODOLOGIES FOR AVERAGE PROBABILITY CALCULATION FOR AEROSPACE SYSTEMS |
ICAS 2008-9.3.3 |
Rand, O. |
GROUND EFFECT MODELING FOR ROTARY-WING SIMULATION |
ICAS 2008-5.11.3 |
Ranieri, A. |
CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE |
ICAS 2008-8.2.1 |
Rasuo, B. |
ON AIRCRAFT PERFORMANCE IMPROVEMENT BY USING WINGLETS |
ICAS 2008-2.8.3 |
Rasuo, B. |
ON RESULTS’ ACCURACY AT TWO-DIMENSIONAL WIND TUNNEL TESTING |
ICAS2008-P2.12 |
Rasuo, B. |
ON-CONDITION MAINTENANCE FOR NON-MODULAR JET ENGINES: AN EXPERIENCE |
ICAS 2008-4.5.2 |
Rathinam, S. |
AN OPTIMIZATION MODEL FOR REDUCING AIRCRAFT TAXI TIMES AT THE DALLAS-FORT WORTH INTERNATIONAL AIRPORT |
ICAS 2008-8.6.1 |
Rauen, A. |
EUROFIGHTER/TYPHOON PROGRAMME |
ICAS 2008-0.5 |
Ravachol, M. |
UNCERTAINTIES AT THE CONCEPTUAL STAGE: MULTILEVEL MULTIDISCIPLINARY DESIGN AND OPTIMIZATION APPROACH |
ICAS 2008-1.1.2 |
Rebentisch, E. |
LEAN PRODUCT DEVELOPMENT IN THE AEROSPACE ENTERPRISE |
ICAS 2008-6.7.1 |
Reckzeh, D. |
AERODYNAMIC DESIGN OF THE A400M HIGH-LIFT SYSTEM |
ICAS 2008-2.7.2 INVITED |
Reed, H. L. |
COMPUTATIONS FOR LAMINAR FLOW CONTROL IN SWEPT-WING BOUNDARY LAYERS |
ICAS 2008-2.7.4 |
Reed, H. L. |
FLIGHT EXPERIMENTS ON SWEPT WING TRANSITION USING DISTRIBUTED ROUGHNESS |
ICAS 2008-2.7.5 |
Régert, T. |
INVESTIGATION ON THE EFFECT OF HYDRODYNAMIC MEMS ON AIRFOIL |
ICAS2008-3.10 ST: |
Rehman, A. |
FRAMEWORK OF PAKISTAN AEROSPACE INDUSTRY QUALITY SYSTEM |
ICAS 2008-6.9.4 |
Reinartz, B. U. |
PERFORMANCE ANALYSIS OF A 3D SCRAMJET INTAKE |
ICAS 2008-4.1.1 |
Reis, M. V. F. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
Renaud, G. |
STATIC AND FATIGUE ANALYSIS OF AN UPPER WING SKIN WITH EXFOLIATION CORROSION |
ICAS 2008-7.4.1 |
Rendall, T. C. S. |
TOWARDS AERODYNAMIC OPTIMISATION OF AN AEROELASTIC WING USING DOMAIN ELEMENT PARAMETERISATION |
ICAS 2008-2.8.1 |
Resende, H. B. |
EVOLUTION OF EMBRAER’S CIVIL AIRCRAFT |
ICAS 2008-1.7.1 INVITED |
Reß, R. |
FIN BUFFET CHARACTERISTICS OF ADVANCED TRAINER AIRCRAFT |
ICAS 2008-3.4.1 |
Reyer, M. |
A WALL SHEAR STRESS MEASUREMENT TECHNIQUE USING THE THERMAL WAKES OF SMALL HEATED SPOTS |
ICAS 2008-3.7.1 |
Reynolds, N. D. |
MODELING OF ACOUSTICALLY TREATED NACELLE LIP TRANSPIRATION FLOW ANTI-ICING SYSTEM |
ICAS 2008-6.4.3 |
Reynolds, T. G. |
ANALYSIS OF LATERAL FLIGHT INEFFICIENCY IN GLOBAL AIR TRAFFIC MANAGEMENT |
ICAS 2008-11.3.1 (AIAA 2008-8865) |
Reynolds, T. G. |
NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY |
ICAS 2008-10.4.4 (AIAA 2008-8890) |
Rezaee, M. |
FEM MICRO-MECHANICAL ANALYSIS OF DELAMINATION PHENOMENON IN IMC LAMINATED COMPOSITES USING DAMAGE THEORY |
ICAS2008-9.4 ST: |
Rhodes, J. |
RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY |
ICAS 2008-8.2.3 |
Rhodes, R. G. |
COMPUTATIONS FOR LAMINAR FLOW CONTROL IN SWEPT-WING BOUNDARY LAYERS |
ICAS 2008-2.7.4 |
Riabov, V. V. |
HEAT TRANSFER ON HYPERSONIC BLUNT BODIES WITH GAS INJECTION |
ICAS 2008-3.6.4 |
Riabov, V. V. |
NUMERICAL AND EXPERIMENTAL STUDIES OF SHOCK INTERFERENCE IN HYPERSONIC FLOWS NEAR A CYLINDER |
ICAS2008-P2.3 |
Riccabone, A. |
METHODOLOGY OPTIMIZATION OF METAL CUTTING PROGRAMMING APPLIED TO AERONAUTICAL COMPONENTS |
ICAS 2008-6.10.5 |
Ricci, S. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
Ricci, S. |
DEVELOPMENT AND VALIDATION OF AN INVESTIGATION TOOL FOR NONLINEAR AEROELASTIC ANALYSIS |
ICAS 2008-9.6.3 |
Ricciardi, J. |
CESSNA CITATION CJ1 FLIGHT TEST DATA GATHERING AND LEVEL-C SIMULATOR MODEL DEVELOPMENT |
ICAS 2008-5.1.2 |
Riccobene, L. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
Rieger, H. |
AERODYNAMIC OPTIMIZATION OF AIRCRAFT CONFIGURATIONS WITH MULTIDISZIPLINARY ASPECTS |
ICAS 2008-2.11.3 |
Riggins, D. |
NUMERICAL STUDY OF ENERGY UTILIZATION IN NOZZLE/PLUME FLOW-FIELDS OF HIGH-SPEED AIR-BREATHING VEHICLES |
ICAS 2008-4.3.3 |
Rihacek, C. |
CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE |
ICAS 2008-8.2.1 |
Rikards, R. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
Rinoie, K. |
VORTEX BEHAVIORS OF CRANKED ARROW WING CONFIGURATIONS WITH DIFFERENT WING PLANFORMS |
ICAS 2008-3.3.2 |
Rinoie, K. |
WING DESIGN OF SUPERSONIC TRANSPORT BY A MULTI-POINT OPTIMIZATION METHOD |
ICAS 2008-2.4.3 |
Rios, J. |
SOLVING HIGH-FIDELITY, LARGE-SCALE TRAFFIC FLOW MANAGEMENT PROBLEMS IN REDUCED TIME |
ICAS 2008-11.7.4 (AIAA 2008-8910) |
Rispoli, A. |
DEVELOPMENT AND TEST OF AN INTEGRATED SENSOR SYSTEM FOR AUTONOMOUS COLLISION AVOIDANCE |
ICAS2008-P6.12 |
Rix, O. |
INNOVATIVE APPROACH FOR FUTURE AIRCRAFT DEVELOPMENT AT IAI |
ICAS 2008-1.6.1 |
Rizzi, A. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
Robinson, R. |
SECURITY ARCHITECTURE AND FORMAL ANALYSIS OF AN AIRPLANE SOFTWARE DISTRIBUTION SYSTEM |
ICAS 2008-9.1.1 |
Robinson, R. |
SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-9.1.3 |
Robinson, R. V. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
Rocha, B. |
ON THE DEVELOPMENT OF METHODS AND TECHNIQUES FOR AIRCRAFT STRUCTURAL HEALTH MONITORING |
ICAS2008-7.4 ST: |
Roget, B. |
PREDICTION OF HELICOPTER MANEUVER LOADS USING A TIGHTLY COUPLED CFD/CSD ANALYSIS |
ICAS 2008-2.10.4 |
Rohács, J. |
FEASIBILITY STUDY ON MULTI-PHASE FLOW SIMULATION OF FUEL INJECTION USING LATTICE BOLTZMANN METHOD |
ICAS 2008-4.3.4 |
Rohács, J. |
INVESTIGATION ON THE EFFECT OF HYDRODYNAMIC MEMS ON AIRFOIL |
ICAS2008-3.10 ST: |
Roling, P. C. |
EVALUATION OF ANCHORAGE INTERNATIONAL AIRPORT USING THE AIRPORT BUSINESS SUITE |
ICAS 2008-10.4.5 (AIAA 2008-8891) |
Roof, C. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Rosa Taddei, S. |
EULER INVERSE THROUGHFLOW MODEL BASED ON AN IMPLICIT UPWIND TIME MARCHING TECHNIQUE |
ICAS 2008-2.3.2 |
Rosenberger, J. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
Ross, H. |
FLY AROUND THE WORLD WITH A SOLAR POWERED AIRPLANE |
ICAS 2008-10.11.1 (AIAA 2008-8954 ) |
Ross, K. |
SOLVING HIGH-FIDELITY, LARGE-SCALE TRAFFIC FLOW MANAGEMENT PROBLEMS IN REDUCED TIME |
ICAS 2008-11.7.4 (AIAA 2008-8910) |
Rouwhorst, W. F. J. A. |
PILOTED SIMULATION RESULTS OF AN ONBOARD WAKE VORTEX DETECTION, WARNING AND AVOIDANCE SYSTEM AND COCKPIT DISPLAY ASPECTS |
ICAS 2008-9.9.1 |
Rowe, D. |
AIRSPACE SECURITY MEASURES EMPLOYED FOR THE UN GENERAL ASSEMBLY MEETING: ANALYSIS AND IMPACT |
ICAS 2008-11.5.1 (AIAA 2008-8892) |
Rozen, N. |
AN AUTOMATED SIMULATION PILOT CAPABILITY TO SUPPORT ADVANCED AIR TRAFFIC CONTROLLER TRAINING |
ICAS 2008-10.5.3 (AIAA 2008-8897) |
Rudolph, I. |
A WALL SHEAR STRESS MEASUREMENT TECHNIQUE USING THE THERMAL WAKES OF SMALL HEATED SPOTS |
ICAS 2008-3.7.1 |
Rudolph, M. |
AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION |
ICAS 2008-8.3.1 |
Ruijgrok, G. J. J. |
ON THE REDUCTION OF NOX-EMISSION LEVELS BY PERFORMING LOW NOX FLIGHTS |
ICAS2008-4.7 ST: |
Rumizen, M. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
Ruzzene, M. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
S., Shinji |
643 DEVELOPMENT OF A COAXIAL ROTOR MAV FOR INDOOR APPLICATION |
ICAS2008-P1.9 |
Saarela, O. |
COMPRESSION STRENGTH OF NOTCHED AND IMPACT DAMAGED COMPOSITE LAMINATES |
ICAS 2008-7.5.2 |
Sachs, G. |
IMPROVEMENT FOR LANDING ON SMALL-MEDIUM AIRPORTS USING FUTURE, AIRCRAFT-AUTONOMOUS GUIDANCE AIDS |
ICAS 2008-5.7.1 INVITED |
Sachs, G. |
TRAJECTORY CONTROL IMPROVEMENT BASED ON A NONLINEAR DYNAMIC INVERSION APPROACH |
ICAS 2008-5.7.2 |
Sachs, G. |
UNIQUE PERFORMANCE CHARACTERISTICS OF SOLAR AIRCRAFT |
ICAS 2008-5.3.2 |
Sachs, H. |
MONITORING OF OSCILLATORY FAILURE CASES FOR THE REDUCTION OF STRUCTURAL LOADS IN AN AEROELASTIC AIRCRAFT |
ICAS 2008-7.7.2 |
Sadraey, M. |
A SYSTEMATIC APPROACH IN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION |
ICAS 2008-1.9.1 (AIAA 2008-8926) |
Safarik, P. |
SEPARATION CONTROL BY SYNTHETIC JET ACTUATOR IN STRAIGHT BLADE CASCADE |
ICAS 2008-3.10.4 |
Saggiani, G. M. |
FLIGHT MECHANICS SIMULATOR FOR ROTORCRAFT DEVELOPMENT |
ICAS2008-P5.4 |
Sainadh, A. |
INCLUSION OF ENGINE RELATED PARAMETERS IN CONCEPTUAL DESIGN OF MORPHING AIRCRAFT |
ICAS 2008-1.6.4 |
Saint-Martin, P. de |
DESIGN OF A SMALL SUPERSONIC TRANSPORT AIRCRAFT WITH HIGH ENVIRONMENTAL CONSTRAINTS |
ICAS 2008-1.10.1 INVITED |
Sala, G. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
Samardzic, M. |
APPLICATION OF SEMICONDUCTOR STRAIN GAUGES IN MEASUREMENTS OF DYNAMIC STABILITY DERIVATIVES IN THE T-38 WIND TUNNEL |
ICAS 2008-3.4.5 |
Samardzic, M. |
PROTOTYPE OF A STIFF WIND TUNNEL BALANCE WITH SEMICONDUCTOR STRAIN GAUGES AND THERMOCOMPENSATION DONE BY SOFTWARE |
ICAS2008-P2.9 |
Sammut, A. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
Sampigethaya, K. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
Sampigethaya, K. |
SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-9.1.3 |
Samuelsson, L. |
FATIGUE ANALYSIS: THE SUPER-NEUBER TECHNIQUE FOR CORRECTION OF LINEAR ELASTIC FE RESULTS |
ICAS 2008-7.4.2 |
Sant, R. |
AERODYNAMIC OPTIMIZATION OF A BLENDED WING BODY |
ICAS2008-2.11 ST: |
Santema, S. C. |
DESIGN OF A LEAN MRO BUSINESS PROCESS FOR EPCOR |
ICAS 2008-10.3.4 (AIAA 2008-8864) |
Santos, L. C. C. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
Saric, W. S. |
COMPUTATIONS FOR LAMINAR FLOW CONTROL IN SWEPT-WING BOUNDARY LAYERS |
ICAS 2008-2.7.4 |
Saric, W. S. |
FLIGHT EXPERIMENTS ON SWEPT WING TRANSITION USING DISTRIBUTED ROUGHNESS |
ICAS 2008-2.7.5 |
Sarma, A. |
AIRSHIP TRANSPORT OPERATIONAL MANAGEMENT IN NORTHERN LATITUDES |
ICAS 2008-10.1.1 (AIAA 2008-8850) |
Sarma, A. |
AN ATMOSPHERIC SIMULATION SYSTEM FOR AVIATION REQUIREMENTS OVER NORTHERN LATITUDES |
ICAS 2008-10.7.2 (AIAA 2008-8915) |
Sato, H. |
OPTIMUM AEROELASTIC DESIGN OF A RESONANCE TYPE FLAPPING WING FOR MICRO AIR VEHICLES |
ICAS 2008-7.10.3 |
Sato, K. |
LOW-BOOM AND LOW-DRAG OPTIMIZATION FOR THE TWIN-ENGINE SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR |
ICAS 2008-2.4.1 |
Scarano, F. |
INVESTIGATION OF THE FLOW IN A RECTANGULAR CAVITY USING TOMOGRAPHIC AND TIME-RESOLVED PIV |
ICAS 2008-3.2.2 |
Schafer, A. |
MODELLING AIRLINE ROUTING AND SCHEDULING UNDER AIRPORT CAPACITY CONSTRAINTS |
ICAS 2008-11.1.2 (AIAA 2008-8855) |
Schäfer, A. |
NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY |
ICAS 2008-10.4.4 (AIAA 2008-8890) |
Schaller, J. |
IMPROVEMENT FOR LANDING ON SMALL-MEDIUM AIRPORTS USING FUTURE, AIRCRAFT-AUTONOMOUS GUIDANCE AIDS |
ICAS 2008-5.7.1 INVITED |
Schaller, J. |
92 LANDING-AVIONIC SYSTEM FOR SMALL-MEDIUM AIRCRAFT FOR AUTOMATED LANDING ON SMALL-MEDIUM AND/OR POORLY EQUIPPED AIRPORTS |
ICAS2008-P6.8 |
Scharl, J. |
ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES |
ICAS 2008-11.9.3 (AIAA 2008-8932) |
Schauenburg, A. |
FLEET MANAGEMENT SYSTEM FOR AN ADVANCED HELICOPTER PLATFORM - DESIGN & DEVELOPMENT REQUIREMENTS |
ICAS 2008-6.11.1 |
Schaufele, R. |
IMPACT OF US-EU OPEN AREA AVIATION TREATY ON US AVIATION: A PARAMETRIC ANALYSIS WITH SIMULATION |
ICAS 2008-10.10.3 (AIAA 2008-8937) |
Scherillo, F. |
SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION |
ICAS 2008-2.7.3 |
Schmid, A. |
FIN BUFFET CHARACTERISTICS OF ADVANCED TRAINER AIRCRAFT |
ICAS 2008-3.4.1 |
Schmidt, M. |
AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION |
ICAS 2008-8.3.1 |
Schmidt, R. C. |
APPLICATION OF THE INTEGRATED PRODUCT TEAM (IPT) CONCEPT TO THE RE-ENGINE OF A VERY LIGHT JET (VLJ) |
ICAS 2008-6.7.5 |
Schmitt, D -R. |
REAL TIME SIMULATION OF INTEGRATION OF UAV'S INTO AIRSPACE |
ICAS 2008-8.1.1 |
Schoemig, E. |
ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES |
ICAS 2008-11.9.3 (AIAA 2008-8932) |
Scholz, D. |
THE GREEN FREIGHTER PROJECT - OBJECTIVES AND FIRST RESULTS |
ICAS 2008-4.10.3 |
Schönfeld, T. |
THE REGIONAL AEROSPACE CLUSTER POLICY IN EUROPE |
ICAS 2008-6.9.2 |
Schreiber, R. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
Schroijen, M. J. T. |
PROPELLER SLIPSTREAM INVESTIGATION USING THE FOKKER F27 WIND TUNNEL MODEL WITH FLAPS DEFLECTED |
ICAS 2008-3.1.2 |
Schuck, F. |
IMPROVEMENT FOR LANDING ON SMALL-MEDIUM AIRPORTS USING FUTURE, AIRCRAFT-AUTONOMOUS GUIDANCE AIDS |
ICAS 2008-5.7.1 INVITED |
Schuster, W. |
SATELLITE-BASED NAVIGATION ARCHITECTURE STUDY FOR AIRCRAFT CATEGORY III LANDINGS |
ICAS 2008-6.4.4 |
Schut, E. J. |
DEVELOPMENT AND IMPLEMENTATION OF KNOWLEDGE-BASED DESIGN PROCESS PRIMITIVES |
ICAS 2008-6.10.4 |
Schwartz, A. |
RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY |
ICAS 2008-8.2.3 |
Schwarz, C. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
Schwarz, C. |
ALLEVIATION OF ATMOSPHERIC FLOW DISTURBANCE EFFECTS ON AIRCRAFT RESPONSE |
ICAS 2008-5.2.2 |
Schwerin, D. |
DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS |
ICAS 2008-6.7.4 |
Scott, M. L. |
LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS |
ICAS 2008-7.2.2 |
Seeckt, K. |
THE GREEN FREIGHTER PROJECT - OBJECTIVES AND FIRST RESULTS |
ICAS 2008-4.10.3 |
Segall, D. |
FLIGHT EVALUATION OF A COMPACT AIRBORNE TRACE GAS ANALYSIS SENSOR PROOF-OF-CONCEPT |
ICAS2008-P6.4 |
Seifert, J. |
A NEW APPROACH FOR CO2 REDUCTION APPLYING STATE-OF-THE-ART ENGINE AND AIRFRAME TECHNOLOGY |
ICAS2008-4.2 ST (AIAA 2008-8974) |
Seifert, J. |
POTENTIALS OF LIGHTER-THAN-AIR TECHNOLOGY IN FUTURE MARKETS – AN EVALUATION |
ICAS2008-P1.7 |
Seifert, J. |
PROMISING FUTURE AIRCRAFT CONCEPT – ESTOL |
ICAS2008-P1.8 |
Seitz, A. |
A NEW APPROACH FOR CO2 REDUCTION APPLYING STATE-OF-THE-ART ENGINE AND AIRFRAME TECHNOLOGY |
ICAS2008-4.2 ST (AIAA 2008-8974) |
Selier, M. |
NATIONAL TECHNOLOGY PROJECT 'OUTCAST' ON UAV SENSE AND AVOID |
ICAS 2008-8.1.2 |
Sénési, S. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
Sengstacken, A. |
UTILIZATION OF NETWORK THEORY FOR THE ENHANCEMENT OF ATO AIR ROUTE FORECAST |
ICAS 2008-11.10.5 (AIAA 2008-8944) |
Sengupta, P. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
Serena Guinzio, P. |
A DUAL-DUPLEX ELECTROHYDRAULIC SYSTEM FOR THE FLY-BY-WIRE CONTROL OF A HELICOPTER MAIN ROTOR |
ICAS 2008-6.6.4 |
Seuschek, H. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
Shah, S. |
PREDICTION OF DELAMINATION IN ADVANCED AEROSPACE COMPOSITE STRUCTURES USING MICRO/MACRO MECHANICS CONSTITUTIVE METHODS |
ICAS 2008-7.5.3 |
Shao, L. M. |
EXPERIMENTAL RESEARCH OF FLAPPING-WING PROPULSION FOR MICRO AIR VEHICLES |
ICAS2008-3.4 ST: |
Shao, P. C. |
IDENTIFYING FATIGUE OF FLIGHT ATTENDANTS IN SHORT-HAUL OPERATIONS |
ICAS 2008-9.2.3 |
Sharma, T. |
ADVANCED METHODOLOGIES FOR AVERAGE PROBABILITY CALCULATION FOR AEROSPACE SYSTEMS |
ICAS 2008-9.3.3 |
Sheth, K. S. |
TASK ANALYSIS FOR FEASIBILITY ASSESSMENT OF A COLLABORATIVE TRAFFIC FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.7.3 (AIAA 2008-8909) |
Shetty, S. |
SYSTEM OF SYSTEMS DESIGN FOR WORLDWIDE COMMERCIAL AIRCRAFT NETWORKS |
ICAS 2008-8.4.1 |
Shi, J. |
NEW METHOD TO ENHANCE THE WEARABILITY OF TITANIUM ALLOY ROTOR BLADE FOR AERO-ENGINE |
ICAS 2008-4.2.4 |
Shin, H. S. |
INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT |
ICAS 2008-5.7.3 |
Shin, H. S. |
NONLINEAR FORMATION GUIDANCE LAW WITH ROBUST DISTURBANCE OBSERVER |
ICAS 2008-5.7.4 |
Shmilovich, A. |
FLOW CONTROL TECHNIQUES FOR TRANSPORT AIRCRAFT |
ICAS 2008-3.11.1 |
Shoji, H. |
IMPACT CHARACTERISTICS ESTIMATION OF SHORT SUPPORT COLUMNS UNDER CABIN FLOOR |
ICAS 2008-9.4.1 |
Sibilski, K. |
FLIGHT SAFETY AS CONSIDERED IN PROBABILISTIC TERMS |
ICAS 2008-9.3.4 |
Sibilski, K. |
MODELING AND SIMULATION OF FLAPPING WINGS MICRO-AERIAL VEHICLES FLIGHT DYNAMICS |
ICAS 2008-5.9.1 INVITED |
Sibilski, K. |
THE INFLUENCE OF FREE - PLAY AND FRICTION IN CONTROL SYSTEM ON AIRCRAFT DYNAMICS |
ICAS 2008-5.10.5 |
Sieber, J. |
"ACTIVE CORE" - A KEY TECHNOLOGY FOR MORE ENVIRONMENTALLY FRIENDLY AERO ENGINES BEING INVESTIGATED UNDER THE NEWAC PROGRAM |
ICAS 2008-4.2.1 |
Sijtsma, P. |
A NOVEL RECIPROCAL SOUND TRANSMISSION MEASURING METHOD, APPLIED ON A COMPOSITE FUSELAGE |
ICAS 2008-4.9.3 |
Siladic, M. F. |
ON-CONDITION MAINTENANCE FOR NON-MODULAR JET ENGINES: AN EXPERIENCE |
ICAS 2008-4.5.2 |
Silva Filho, D. H. |
EVOLUTION OF EMBRAER’S CIVIL AIRCRAFT |
ICAS 2008-1.7.1 INVITED |
Silva, A. L. da |
A PROCEDURE TO DESIGN AIRCRAFT FLIGHT CONTROL LAWS TAKING INTO ACCOUNT ROBUSTNESS USING THE VARIABLE STRUCTURE CONTROL |
ICAS2008-5.4 ST: |
Silva, R. F. A. F. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
Simeonides, G. A. |
LAMINAR-TURBULENT TRANSITION CORRELATION IN SUPERSONIC/ HYPERSONIC FLOW – ATTACHED VERSUS SEPARATED FLOW |
ICAS 2008-3.8.3 |
Singh, C. |
AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS |
ICAS 2008-3.11.3 |
Sinha, A. |
DESIGN OF A NOVEL INTELLIGENT DATA MANAGEMENT TOOL FOR HEALTH AND USAGE MONITORING SYSTEMS – DESIGN REQUIREMENTS |
ICAS2008-6.1 ST: |
Sinha, A. K. |
EVALUATION OF AN INTEROPERABLE VERTICAL TAKE-OFF UAV FOR OPERATIONS WITH UGVS - AN OVERVIEW |
ICAS 2008-6.11.2 |
Sinha, A. K. |
FLEET MANAGEMENT SYSTEM FOR AN ADVANCED HELICOPTER PLATFORM - DESIGN & DEVELOPMENT REQUIREMENTS |
ICAS 2008-6.11.1 |
Sitaraman, J. |
PREDICTION OF HELICOPTER MANEUVER LOADS USING A TIGHTLY COUPLED CFD/CSD ANALYSIS |
ICAS 2008-2.10.4 |
Slingerland, R. |
PROPELLER SLIPSTREAM INVESTIGATION USING THE FOKKER F27 WIND TUNNEL MODEL WITH FLAPS DEFLECTED |
ICAS 2008-3.1.2 |
Smaili, M. H. |
A SIMULATION BENCHMARK FOR AIRCRAFT SURVIVABILITY ASSESSMENT |
ICAS 2008-9.3.2 |
Smaili, M. H. |
OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION |
ICAS 2008-2.11.2 |
Smid, R. |
EMAT APPLIED IN THE AVIATION INDUSTRY |
ICAS2008-P1.1 (AIAA 2008-8870) |
Smith, A. |
AN ADAPTABLE METHODOLOGY FOR AUTOMATION APPLICATION DEVELOPMENT |
ICAS 2008-6.2.3 |
Smith, A. P. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
Smith, B. E. |
A PROGNOSTIC METHOD TO IDENTIFY HAZARDS FOR FUTURE AVIATION CONCEPTS |
ICAS 2008-9.3.1 |
Smith, E. |
OPERATIONAL ACCEPTABILITY OF ISSUING RNAV/RNP PROCEDURE CHANGES IN FUTURE TERMINAL ENVIRONMENTS |
ICAS2008-11.8 ST (AIAA 2008-8922) |
Smith, H. |
NOVEL DESIGN CONCEPTS FOR AIRCRAFT WITH REDUCED NOISE AND GLOBAL WARMING CHARACTERISTICS |
ICAS 2008-4.10.4 |
Smith, J. C. |
A PERFORMANCE ASSESSMENT OF A TACTICAL AIRBORNE SEPARATION ASSISTANCE SYSTEM USING REALISTIC, COMPLEX TRAFFIC FLOWS |
ICAS 2008-11.4.4 (AIAA 2008-8884) |
Smith, N. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
Smrcek, L. |
PERFORMANCE DEGRADATION OF A SIMULATED ICE CONTAMINATED AIRFOIL BY SUPER-COOLED DROPLETS |
ICAS 2008-3.7.2 |
Sobester, A. |
THE QUEST FOR A TRULY PARSIMONIOUS AIRFOIL PARAMETERIZATION SCHEME |
ICAS2008-P2.2 (AIAA 2008-8879) |
Soedarsono, A. A. |
DEVELOPMENT OF UNMANNED AERIAL VEHICLE IN BPPT |
ICAS2008-P1.10 |
Sohn, M. |
DELTA-WING VORTEX CONTROL BY APEX STRAKE AND MICRO LEADING-EDGE FLAP |
ICAS2008-3.3 ST: |
Sollo, A. |
FE STUDY OF WINDSHIELD SUBJECTED TO HIGH SPEED BIRD IMPACT |
ICAS 2008-9.4.3 |
Solomos, G. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
Somos, M. |
PARAMETER IDENTIFICATION OF FLYING WING WITH SIGNIFICANT DEFORMATION |
ICAS 2008-5.8.1 |
Song, B. |
DEVELOPMENT OF FLAPPING WING MICRO AIR VEHICLE |
ICAS 2008-1.5.3 |
Song, B. F. |
COORDINATELY MODELING AND SIMULATION OF THE EJECTION SEAT/OCCUPANT SYSTEM |
ICAS2008-P9.3 |
Song, B. F. |
ERGONOMIC ASSESSMENT METHOD FOR COCKPIT LAYOUT OF CIVIL AIRCRAFT X BASED ON VIRTUAL DESIGN |
ICAS2008-P6.5 |
Song, B. F. |
EXPERIMENTAL RESEARCH OF FLAPPING-WING PROPULSION FOR MICRO AIR VEHICLES |
ICAS2008-3.4 ST: |
Song, B. F. |
HEALTH MONITORING FOR AEROCRAFT STRUCTURE SYSTEM BY HARMONIC WAVELET TRANSFORM |
ICAS2008-7.7 ST: |
Song, B. F. |
LOW REYNOLDS NUMBER TANDEM OR DIAMOND WING UAV AERODYNAMICS CENTER RESEARCH BASED ON RESPONSE SURFACE METHOD |
ICAS2008-3.1 ST: |
Song, B. F. |
METHODS FOR CALCULATING THE DAMAGE-RATE OF AIRCRAFT COMPONENT |
ICAS2008-9.8 ST: |
Song, B. F. |
NUMERICAL SIMULATION OF 3D FLAPPING WING BASED ON CHIMERA METHOD |
ICAS 2008-2.10.5 |
Song, B. F. |
THE SIMULATION OF THE HUMAN-MACHINE PARTNERSHIP IN UCAV OPERATION |
ICAS 2008-9.10.5 |
Song, K. |
LIFT PREDICTION OF MULTI-ELEMENT AIRFOIL USING DES AND RANS |
ICAS2008-P2.5 |
Song, L. |
METHODOLOGIES FOR ESTIMATING THE IMPACT OF SEVERE WEATHER ON AIRSPACE CAPACITY |
ICAS 2008-10.7.4 (AIAA 2008-8917) |
Song, W. P. |
NUMERICAL SIMULATION OF 3D FLAPPING WING BASED ON CHIMERA METHOD |
ICAS 2008-2.10.5 |
Soper, T. J. |
DRAG AND FLOW REGIMES ASSOCIATED WITH RECTANGULAR CAVITIES AT YAW AT LOW SPEEDS |
ICAS2008-P2.13 |
Sorensen, K. |
AERODYNAMIC OPTIMIZATION OF AIRCRAFT CONFIGURATIONS WITH MULTIDISZIPLINARY ASPECTS |
ICAS 2008-2.11.3 |
Sorli, M. |
A DUAL-DUPLEX ELECTROHYDRAULIC SYSTEM FOR THE FLY-BY-WIRE CONTROL OF A HELICOPTER MAIN ROTOR |
ICAS 2008-6.6.4 |
Spadoni, A. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
Spano, E. |
EULER INVERSE THROUGHFLOW MODEL BASED ON AN IMPLICIT UPWIND TIME MARCHING TECHNIQUE |
ICAS 2008-2.3.2 |
Speciale, G. |
TRAJECTORY OPTIMISATION FOR AUTONOMOUS VEHICLES: A MINIUAV APPLICATION |
ICAS 2008-5.6.3 |
Speidel, J. |
INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS |
ICAS 2008-8.4.5 |
Spence, G. T. |
REAL-TIME SIMULATION OF A DISTRIBUTED CONFLICT RESOLUTION ALGORITHM |
ICAS 2008-8.7.3 |
Spies, G. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
Spiker, M. A. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
Spogis, N. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
Sproewitz, T. |
THERMAL ASPECTS FOR COMPOSITE STRUCTURES - FROM MANUFACTURING TO IN-SERVICE PREDICTIONS |
ICAS 2008-7.9.4 |
Sprong, K. P. |
IMPROVING TERMINAL OPERATIONS - BENEFITS OF RNAV DEPARTURE PROCEDURES AT DALLAS-FORT WORTH AND HARTSFIELD-JACKSON ATLANTA INTERNATIONAL AIRPORTS |
ICAS 2008-11.1.3 (AIAA 2008-8856) |
Sridar, B. |
ESTIMATION OF AIR TRAFFIC DELAY USING THREE DIMENSIONAL WEATHER INFORMATION |
ICAS 2008-10.7.3 (AIAA 2008-8916) |
Sridhar, B. |
PREDICTION OF WEATHER-RELATED DELAYS IN THE CONTINENTAL UNITED STATES |
ICAS 2008-8.2.2 |
Srinivasan, R. |
FLIGHT EVALUATION OF A COMPACT AIRBORNE TRACE GAS ANALYSIS SENSOR PROOF-OF-CONCEPT |
ICAS2008-P6.4 |
Stalnaker, S. |
INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.10.1 (AIAA 2008-8940) |
Stamm, R. |
NETWORK ENABLED OPERATIONS ENHANCES AVIATION EFFICIENCY |
ICAS 2008-8.8.1 (AIAA 2008-8951) |
Stanek, M. |
IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT |
ICAS 2008-2.6.2 |
Stapleton, S. |
INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.10.1 (AIAA 2008-8940) |
Starik, A. |
INNOVATIONS IN COMBUSTION TECHNOLOGY FOR PROPULSION |
ICAS 2008-0.6 |
Stassen, H. P. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
Stefanik, M. |
CAPACITY RESEARCH OF BRNO-TURANY AIRPORT WITH RESPECT TO NEW TRENDS IN AIR TRANSPORT |
ICAS 2008-8.5.3 |
Steigenberge, J. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
Steinkellner, S. |
HOSTED SIMULATION FOR HETEROGENEOUS AIRCRAFT SYSTEM DEVELOPMENT |
ICAS2008-6.2 ST: |
Stoica, A.-M. |
AUTOMATIC FLIGHT CONTROL USING SAMPLED-DATA MIXED H_2/H_INFINITY OPTIMISATION |
ICAS 2008-5.2.1 |
Stoufflet, B |
DESIGN OF A SMALL SUPERSONIC TRANSPORT AIRCRAFT WITH HIGH ENVIRONMENTAL CONSTRAINTS |
ICAS 2008-1.10.1 INVITED |
Streit, T. |
ACTIVE AND PASSIVE STRUCTURAL MEASURES FOR AEROELASTIC WINGLET DESIGN |
ICAS 2008-7.10.1 |
Stroosma, O. |
A SIMULATION BENCHMARK FOR AIRCRAFT SURVIVABILITY ASSESSMENT |
ICAS 2008-9.3.2 |
Strybel, T. Z. |
COMPARING SITUATION AWARENESS MEASUREMENT TECHNIQUES IN A LOW FIDELITY AIR TRAFFIC CONTROL SIMULATION |
ICAS 2008-9.7.4 |
Stuip, M. |
NATIONAL TECHNOLOGY PROJECT 'OUTCAST' ON UAV SENSE AND AVOID |
ICAS 2008-8.1.2 |
Stumpf, E. |
A HOLISTIC APPROACH TO EVALUATE THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-8.4.2 |
Styuart, A. V. |
PROBABILISTIC MODELING OF STRUCTURAL / AEROELASTIC LIFE CYCLE FOR RELIABILITY EVALUATION OF DAMAGE TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.1.1 |
Su, J. M. |
LOW REYNOLDS NUMBER TANDEM OR DIAMOND WING UAV AERODYNAMICS CENTER RESEARCH BASED ON RESPONSE SURFACE METHOD |
ICAS2008-3.1 ST: |
Su, R. E. |
ERGONOMIC ASSESSMENT METHOD FOR COCKPIT LAYOUT OF CIVIL AIRCRAFT X BASED ON VIRTUAL DESIGN |
ICAS2008-P6.5 |
Subbarao, K. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
Subbarao, K. |
TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.1.1 (AIAA 2008-8854) |
Suikat, R. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
Sulaeman, E. |
646 ANALYTICAL FORMULATION FOR NON-UNIFORM BEAM FINITE ELEMENT |
ICAS2008-P3.10 |
Suleman, A. |
ON THE DEVELOPMENT OF METHODS AND TECHNIQUES FOR AIRCRAFT STRUCTURAL HEALTH MONITORING |
ICAS2008-7.4 ST: |
Sumi, T. |
HIGH-ORDER LARGE EDDY SIMULATION AROUND 2-D AEROFOIL WITH HIGH-LIFT DEVICE |
ICAS 2008-2.1.2 |
Sumi, T. |
INTERFACE CONDITIONS OF FINITE-DIFFERENCE COMPACT SCHEMES FOR COMPUTATIONAL AEROACOUSTICS |
ICAS 2008-2.3.1 |
Sumi, T. |
LARGE EDDY SIMULATION AROUND 2-D AIRFOIL WITH NATURAL TRANSITION AT HIGH REYNOLDS NUMBERS |
ICAS2008-2.1 ST: |
Sun, C. |
OPTIMIZATION DESIGN ON PLATE-RIB STRUCTURE FOR CERTAIN KINDS OF AIRCRAFT |
ICAS 2008-9.5.3 |
Sun, D. C. |
CFD RESEARCH FOR AIR-TO-AIR MISSILE WITH LATERAL JET CONTROL |
ICAS2008-2.64 ST: |
Sun, L. |
ADAPTING THE ACCIMAP FOR AN ANALYSIS OF THE SQ006 ACCIDENT |
ICAS2008-P9.1 (AIAA 2008-8878) |
Sun, Q. |
STUDY ON THE RELATIONSHIP BETWEEN CORROSION DAMAGE AND RESIDUAL STRENGTH OF AL 7075-T6 ALLOY |
ICAS 2008-9.8.2 |
Sun, W. |
PROMISING FUTURE AIRCRAFT CONCEPT – ESTOL |
ICAS2008-P1.8 |
Sun, Y. F. |
THE SYSTEM FAULT BEHAVIOR AND MODEL |
ICAS2008-P9.2 |
Sun, Y. J. |
THE APPLICATION OF THE MORLET WAVELET ON RESPONSE FILTERING OF THE HELICOPTER CANNON’S RECOIL |
ICAS2008-P3.5 |
Sunderlin, J. |
OPERATIONAL ASSESSMENT OF THE INTEGRATED TERMINAL WEATHER SYSTEM (ITWS) USING DIRECT MEASUREMENT |
ICAS 2008-10.7.5 (AIAA 2008-8918) |
Surace, C. |
A NEGATIVE SELECTION APPROACH TO DETECT DAMAGE IN AERONAUTICAL STRUCTURES WITH CHANGING OPERATING CONDITIONS |
ICAS 2008-9.4.2 |
Surace, G. |
A NEGATIVE SELECTION APPROACH TO DETECT DAMAGE IN AERONAUTICAL STRUCTURES WITH CHANGING OPERATING CONDITIONS |
ICAS 2008-9.4.2 |
Sutherland, A. N. |
A SMALL SCALE PITCH-PLUNGE FLUTTER MODEL FOR ACTIVE FLUTTER CONTROL RESEARCH |
ICAS 2008-3.4.4 |
Suzuki, H. |
TRAJECTORY DESIGN OF SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR (S3TD) |
ICAS 2008-5.7.5 |
Suzuki, S. |
HARMONIZING AUTOMATION, PILOT AND AIR TRAFFIC CONTROLLER IN THE FUTURE AIR TRAFFIC MANAGEMENT |
ICAS 2008-8.2.4 |
Suzuki, S. |
RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM – PART 1. INTELLIGENT FLIGHT CONTROL SYSTEM |
ICAS 2008-5.10.1 |
Suzuki, S. |
ROBUST OPTIMAL DESIGN OF AN AUTOPILOT FOR TRANSITIONAL FLIGHTS OF A TAIL-SITTER MINI UAV |
ICAS 2008-5.9.2 |
Sweers, G. J. |
RECENT DEVELOPMENTS OF MSG-3 (MAINTANANCE STEERING GROUP) GUIDANCE FOR THE CONTINUED AIRWORTHINESS OF LIGHTNING/HIRF PROTECTION AND BENFITS TO NEW AIRPLANE DESIGN |
ICAS 2008-9.4.5 (AIAA 2008-8964 ) |
Szasz, S. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
Szilder, K. |
PREDICTION OF SUPERCOOLED DROPLET IMPINGEMENT ON HELICOPTER ROTOR BLADES |
ICAS 2008-2.6.4 |
Szurgyi, S. |
DEFINITION AND DEMONSTRATION OF THE AIRCRAFT PERFORMANCE EVALUATION CAPABILITIES (APECS) TOOL |
ICAS 2008-11.2.3 (AIAA 2008-8859) |
Tabary, P. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
Tafferner, A. |
AN INTEGRATED USER-ORIENTED WEATHER FORECAST SYSTEM FOR AIR TRAFFIC USING REAL-TIME OBSERVATIONS AND MODEL DATA |
ICAS 2008-8.6.3 |
Tafferner, A. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
Tahk, M. J |
NONLINEAR FORMATION GUIDANCE LAW WITH ROBUST DISTURBANCE OBSERVER |
ICAS 2008-5.7.4 |
Tahk, M. J. |
INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT |
ICAS 2008-5.7.3 |
Tahk, M. J. |
OPTIMIZATION FOR FLIGHT CONTROL SYSTEM WITH CONSTRAINTS SUPPLEMENTED HANDLING QUALITIES |
ICAS 2008-5.3.4 |
Tahk, M. J. |
PERFORMANCE EVALUATION AND HILS TEST OF CONTROL ALLOCATION METHODS FOR RECONFIGURATION CONTROL |
ICAS 2008-5.10.3 |
Takagi, S. |
RELATION BETWEEN TRAILING EDGE NOISE AND BOUNDARY LAYER INSTABILITY |
ICAS2008-P2.14 |
Takeda, N. |
RECENT DEVELOPMENT OF STRUCTURAL HEALTH MONITORING TECHNOLOGIES FOR AIRCRAFT COMPOSITE STRUCTURES |
ICAS 2008-0.7 |
Takenaka, K. |
MULTI-DISCIPLINARY DESIGN EXPLORATION FOR WINGLET |
ICAS 2008-1.1.3 |
Tamada, I. |
NUMERICAL STUDY OF THE EFFECT OF THE OPPOSING JET ON REDUCTION OF AERODYNAMIC HEATING WITH DIFFERENT NOSE CONFIGURATIONS |
ICAS 2008-3.6.3 |
Tan, X. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
Tanaka, H. |
DEVELOPMENT OF AN ONBOARD DOPPLER LIDAR FOR FLIGHT SAFETY |
ICAS 2008-9.9.2 |
Tanaka, K. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
Tandale, M. D. |
MODEL-BASED AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.1 (AIAA 2008-8907) |
Tandale, M. D. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
Tandale, M. D. |
RAPID PREDICTION OF AIR TRAFFIC FOR TRAJECTORY BASED OPERATIONS |
ICAS2008-11.6 ST (AIAA 2008-8902) |
Tang, F. C. |
THE APPLICATION OF SEMI-EMPIRICAL STORE RELEASE SIMULATION FOR THE OPTIMIZATION OF GRID SURVEY WIND TUNNEL TESTING |
ICAS 2008-3.1.3 |
Tang, H. |
EXTENDING FMC TEST FOR FLIGHT SIMULATION AND FLIGHT EXPERIMENTS |
ICAS 2008-5.5.3 |
Tang, N. |
TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT |
ICAS 2008-2.9.2 |
Tani, Y. |
CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION |
ICAS 2008-1.2.3 |
Tani, Y. |
NUMERICAL STUDY OF THE EFFECT OF THE OPPOSING JET ON REDUCTION OF AERODYNAMIC HEATING WITH DIFFERENT NOSE CONFIGURATIONS |
ICAS 2008-3.6.3 |
Taniguchi, H. |
ANALYSIS OF DEEPSTALL LANDING FOR UAV |
ICAS 2008-5.6.4 |
Tarakan, R. |
AN AUTOMATED SIMULATION PILOT CAPABILITY TO SUPPORT ADVANCED AIR TRAFFIC CONTROLLER TRAINING |
ICAS 2008-10.5.3 (AIAA 2008-8897) |
Tarkian, M. |
AIRCRAFT PARAMETRIC 3D MODELING AND PANEL CODE ANALYSIS FOR CONCEPTUAL DESIGN |
ICAS2008-P1.3 |
Taylor, R. M. |
METHODOLOGY FOR THERMALLY INDUCED LOADING IN STRUCTURAL ANALYSIS ON THE F-35 LIGHTNING II |
ICAS 2008-7.11.1 |
Teimouri, H. |
EFFECTS OF HIERARCHY ORDER ON NATURAL FREQUENCY AND VIBRATION TRANSMISSION OF SELF-SIMILAR TRUSSES |
ICAS2008-P3.9 |
Tessier, F. J. Z. |
AIRCRAFT PARAMETRIC 3D MODELING AND PANEL CODE ANALYSIS FOR CONCEPTUAL DESIGN |
ICAS2008-P1.3 |
Tessmer, J. |
COLLAPSE BEHAVIOR OF THIN-WALLED CFRP STRUCTURES DUE TO MATERIAL AND GEOMETRIC NONLINEARITIES–EXPERIMENTS AND SIMULATION |
ICAS 2008-7.11.3 |
Tessmer, J. |
IMPACT RESISTANCE, DAMAGE TOLERANCE AND NON-DESTRUCTIVE DAMAGE DETECTION FOR SANDWICH STRUCTURES: ANALYSIS AND TESTING |
ICAS2008-7.5 ST: |
Tessmer, J. |
MECHANICS OF COMPOSITES IN LIGHTWEIGHT STRUCTURES: EFFICIENT TESTING AND COMPUTATION ACCOUNTING FOR COMPLEX 3D BEHAVIOUR |
ICAS 2008-7.11.2 |
Tessmer, J. |
THERMAL ASPECTS FOR COMPOSITE STRUCTURES - FROM MANUFACTURING TO IN-SERVICE PREDICTIONS |
ICAS 2008-7.9.4 |
Thalin, P. |
PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES |
ICAS2008-6.6 ST (AIAA 2008-8973) |
Thielecke, F. |
EVAPORATING COOLANT FOR ON-BOARD COOLING SYSTEMS WITH DIRECT CONDENSATION THROUGH AMBIENT AIR |
ICAS 2008-6.6.3 |
Thielecke, F. |
MONITORING OF OSCILLATORY FAILURE CASES FOR THE REDUCTION OF STRUCTURAL LOADS IN AN AEROELASTIC AIRCRAFT |
ICAS 2008-7.7.2 |
Thielecke, F. |
MULTIVARIABLE CONTROLLER DESIGN FOR A TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WITH TWO PRIMARY LOAD PATHS |
ICAS 2008-6.4.2 |
Thien, H.C. |
643 DEVELOPMENT OF A COAXIAL ROTOR MAV FOR INDOOR APPLICATION |
ICAS2008-P1.9 |
Thipphavong, D. |
AUTOMATED SEPARATION ASSURANCE IN THE PRESENCE OF UNCERTAINTY |
ICAS 2008-8.11.1 |
Thomas, D. G. |
DESIGN ANALYSIS OF AN AIRCRAFT PARACHUTE RECOVERY SYSTEM FOR VERY LIGHT JETS |
ICAS2008-1.11 ST (AIAA 2008-8949) |
Thomas, D. G. |
DEVELOPMENT OF A LANDING DRAG CHUTE SYSTEM SYSTEM FOR VERY LIGHT JETS |
ICAS 2008-1.11.3 (AIAA 2008-8950) |
Thomas, J. P. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
Thomas, R. L. |
DESIGN ANALYSIS OF AN AIRCRAFT PARACHUTE RECOVERY SYSTEM FOR VERY LIGHT JETS |
ICAS2008-1.11 ST (AIAA 2008-8949) |
Thomas, R. L. |
DEVELOPMENT OF A LANDING DRAG CHUTE SYSTEM SYSTEM FOR VERY LIGHT JETS |
ICAS 2008-1.11.3 (AIAA 2008-8950) |
Thomson, R. |
INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS |
ICAS 2008-7.2.1 |
Thomson, R. S. |
THE DESIGN OF POSTBUCKLING COMPOSITE AEROSPACE STRUCTURES ACCOUNTING FOR DAMAGE INITIATION AND GROWTH |
ICAS 2008-7.3.2 |
Thouault, N. |
AERODYNAMIC INVESTIGATIONS ON A GENERIC FAN-IN-WING CONFIGURATION |
ICAS 2008-3.5.1 |
Tian, F. L. |
RESEARCH ON FUZZY LOGIC PIO DETECTOR |
ICAS 2008-5.4.5 |
Tilmann, C. P. |
SUPERSONIC AIRCRAFT FORMATION FLYING TO INCREASE FLIGHT EFFICIENCY |
ICAS 2008-1.10.2 |
Toebben, H. H. |
INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS |
ICAS 2008-8.4.5 |
Tomita, H. |
RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM - PART 2 FLIGHT EXPERIMENTS |
ICAS 2008-5.10.2 |
Torkamani, S. |
SCALED DOWN MODELS FOR FREE VIBRATION ANALYSIS OF ORTHOGONALLY STIFFENED CYLINDRICAL SHELLS USING SIMILITUDE THEORY |
ICAS 2008-7.7.5 |
Torres, J. |
ON-DEMAND SPECIAL USE AIRSPACE |
ICAS 2008-10.10.4 (AIAA 2008-8938) |
Torres, L. A. B. |
DEVELOPMENT OF A SMALL UNMANNED AIR VEHICLE WITH MINIMUM SENSORS PHILOSOPHY |
ICAS2008-1.4 ST: |
Towers, G. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
Townsend, S. |
COUPLED HIGH-FIDELITY ENGINE SYSTEM SIMULATION |
ICAS 2008-8.10.3 INVITED |
Tranchero, B. |
ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT |
ICAS2008-6.6 ST: |
Trapani, M. |
DEVELOPMENT OF A RUDDERLESS AEROELASTIC FIN TECHNOLOGY |
ICAS 2008-7.10.2 |
Trimmel, M. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
Trot, G. |
PRELIMINARY GUIDELINES ON FLIGHT DECK PROCEDURES FOR VERY CLOSELY SPACED PARALLEL APPROACHES |
ICAS 2008-8.5.2 |
Trujillo, A. |
INFORMATION REQUIREMENTS FOR SUPERVISORY AIR TRAFFIC CONTROLLERS IN SUPPORT OF A MID-TERM WAKE VORTEX DEPARTURE SYSTEM |
ICAS 2008-8.11.3 |
Trunk, M. |
LONG TERM AIRCRAFT PROJECT AND TECHNOLOGY EVALUATION UNDER THE UNCERTAINTY OF FUTURE SCENARIOS |
ICAS 2008-1.3.4 |
Tsach, S. |
INNOVATIVE APPROACH FOR FUTURE AIRCRAFT DEVELOPMENT AT IAI |
ICAS 2008-1.6.1 |
Tsourdos, A. |
INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT |
ICAS 2008-5.7.3 |
Tsuda, H. |
CBAQ: DEVELOPMENT OF CRM BEHAVIOR ANALYSIS METHOD FOR MISSION FLIGHT CREW TRAINING |
ICAS 2008-9.2.1 |
Tunney, J. |
FLIGHT EVALUATION OF A COMPACT AIRBORNE TRACE GAS ANALYSIS SENSOR PROOF-OF-CONCEPT |
ICAS2008-P6.4 |
Turner, M. |
COUPLED HIGH-FIDELITY ENGINE SYSTEM SIMULATION |
ICAS 2008-8.10.3 INVITED |
Turp, D. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
Twig, D. |
ADVANCED METHODOLOGIES FOR AVERAGE PROBABILITY CALCULATION FOR AEROSPACE SYSTEMS |
ICAS 2008-9.3.3 |
Tysell, L. |
EXPERIENCES OF GRID GENERATION AND STEADY/UNSTEADY VISCOUS COMPUTATIONS FOR COMPLEX GEOMETRIES |
ICAS 2008-2.5.2 |
Uebersax, A. |
STATIC AND FATIGUE ANALYSIS OF AN UPPER WING SKIN WITH EXFOLIATION CORROSION |
ICAS 2008-7.4.1 |
Unger, R. |
NUMERICAL ANALYSIS OF THIN-WALLED STRUCTURES IN HYPERSONIC FLOW REGIME |
ICAS 2008-3.6.1 |
Unger, R. |
NUMERICAL SIMULATION OF AN OSCILLATING AND FLEXIBLE AIRFOIL FOR FLAPPING WING PROPULSION WITH FLUID-STRUCTURE INTERACTION |
ICAS 2008-7.10.4 |
Ura, H. |
AEROACOUSTIC NOISE MEASUREMENTS IN AERODYNAMIC LOW-SPEED WIND TUNNELS |
ICAS 2008-3.2.3 |
Ura, H. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
Urik, T. |
INNOVATIVE COMPOSITE STRUCTURES FOR SMALL AIRCRAFT |
ICAS2008-7.3 ST: |
Urvoy, C. |
SIMULATOR EVALUATION OF A NOVEL SURFACE MOVEMENT AWARENESS AND ALERTING SYSTEM (SMAAS) FOR RUNWAY INCURSION AVOIDANCE |
ICAS 2008-11.11.2 (AIAA 2008-8959) |
Usdrowski, S. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
Utsch, R. L. de F. P. |
580 A MULTIDISCIPLINARY OPTIMIZATION METHOD APPLIED TO AIRCRAFT DESIGN |
ICAS2008-P1.4 |
Valmorisco, M. |
SAFE AUTOMATIC FLIGHT BACK AND LANDING OF AIRCRAFT (SOFIA) |
ICAS2008-9.7 ST: |
van Dalen, F. |
AUTOMATING THE DEVELOPMENT PROCESS OF THERMOPLASTIC COMPOSITE SHEET RIBS USING KNOWLEDGE BASED ENG. TECHNIQUES |
ICAS 2008-6.10.3 |
van Dartel, I. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
van de Vijver, Y. A. J. R. |
ENVIRONMENT-AWARE RUNWAY ALLOCATION ADVICE SYSTEM |
ICAS 2008-4.11.2 |
van den Hoven, M. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
van der Elst, S. W. G. |
DOMAIN SPECIFIC MODELING LANGUAGES TO SUPPORT MODEL-DRIVEN ENGINEERING OF AIRCRAFT SYSTEMS |
ICAS 2008-1.9.2 (AIAA 2008-8927) |
van der Heul, D. R. |
OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION |
ICAS 2008-2.11.2 |
van der Laan, T. |
AUTOMATING THE DEVELOPMENT PROCESS OF THERMOPLASTIC COMPOSITE SHEET RIBS USING KNOWLEDGE BASED ENG. TECHNIQUES |
ICAS 2008-6.10.3 |
van der Steen, M. |
THE APPLICATION OF SEMI-EMPIRICAL STORE RELEASE SIMULATION FOR THE OPTIMIZATION OF GRID SURVEY WIND TUNNEL TESTING |
ICAS 2008-3.1.3 |
Van der Velden, C. |
AN ADAPTABLE METHODOLOGY FOR AUTOMATION APPLICATION DEVELOPMENT |
ICAS 2008-6.2.3 |
van der Wal, H. |
A NOVEL RECIPROCAL SOUND TRANSMISSION MEASURING METHOD, APPLIED ON A COMPOSITE FUSELAGE |
ICAS 2008-4.9.3 |
van Eenige, M. J. A. |
A PRACTICAL APPROACH TO MULTI-OBJECTIVE CAPACITY ANALYSIS OF AN ENVIRONMENT-AWARE AIRPORT |
ICAS 2008-8.5.1 |
van Gerwen, D. J. |
A NEW APPROACH TO FORCED FLAPPING FOR THE ORNICOPTER |
ICAS 2008-10.11.3 (AIAA 2008-8975) |
van Holten, T. |
A NEW APPROACH TO FORCED FLAPPING FOR THE ORNICOPTER |
ICAS 2008-10.11.3 (AIAA 2008-8975) |
van Holten, T. |
FEASIBILITY ANALYSIS OF ACHIEVING A STABILIZED APPROACH |
ICAS 2008-5.4.2 |
van Muijden, J. |
EFFICIENT AEROELASTIC SIMULATION IN A PARAMETRIC PROCEDURE FOR FATIGUE ANALYSIS |
ICAS 2008-7.7.1 |
Van Putten, B. -J. |
AN ONTOLOGY FOR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-9.11.1 (AIAA 2008-8946) |
van Tooren, M. J. L. |
DEVELOPMENT AND IMPLEMENTATION OF KNOWLEDGE-BASED DESIGN PROCESS PRIMITIVES |
ICAS 2008-6.10.4 |
van Tooren, M. J. L. |
DOMAIN SPECIFIC MODELING LANGUAGES TO SUPPORT MODEL-DRIVEN ENGINEERING OF AIRCRAFT SYSTEMS |
ICAS 2008-1.9.2 (AIAA 2008-8927) |
van Tooren, M. J. L. |
KNOWLEDGE BASED ENGINEERING TO SUPPORT AIRCRAFT MULTIDISCIPLINARY DESIGN AND OPTIMISATION |
ICAS 2008-6.10.1 |
Van Tooren, M. J. L. |
MDO DESIGN SUPPORT BY INTEGRATED ENGINEERING SERVICES WITHIN A MULTI-AGENT TASK ENVIRONMENT |
ICAS 2008-1.11.1 (AIAA 2008-8947) |
Vankan, W. J. |
A PRACTICAL APPROACH TO MULTI-OBJECTIVE CAPACITY ANALYSIS OF AN ENVIRONMENT-AWARE AIRPORT |
ICAS 2008-8.5.1 |
Vargas, F. J. T. |
A PROCEDURE TO DESIGN AIRCRAFT FLIGHT CONTROL LAWS TAKING INTO ACCOUNT ROBUSTNESS USING THE VARIABLE STRUCTURE CONTROL |
ICAS2008-5.4 ST: |
Veldhuis, L. L. M. |
PROPELLER SLIPSTREAM INVESTIGATION USING THE FOKKER F27 WIND TUNNEL MODEL WITH FLAPS DEFLECTED |
ICAS 2008-3.1.2 |
Veldhuis, L. L. M. |
VORTEX WAKE INVESTIGATION BEHIND A WING-FLAP MODEL WITH JET SIMULATION |
ICAS 2008-3.9.1 |
Vera-Morales, M. |
NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY |
ICAS 2008-10.4.4 (AIAA 2008-8890) |
Veress, A. |
FEASIBILITY STUDY ON MULTI-PHASE FLOW SIMULATION OF FUEL INJECTION USING LATTICE BOLTZMANN METHOD |
ICAS 2008-4.3.4 |
Verhoeff, L. |
ENABLING TECHNOLOGY EVALUATION FOR EFFICIENT CONTINUOUS DESCENT APPROACHES |
ICAS 2008-8.9.2 |
Verhoeven, R. P. M. |
ENABLING TECHNOLOGY EVALUATION FOR EFFICIENT CONTINUOUS DESCENT APPROACHES |
ICAS 2008-8.9.2 |
Verhoeven, R. P. M. |
NATIONAL TECHNOLOGY PROJECT 'OUTCAST' ON UAV SENSE AND AVOID |
ICAS 2008-8.1.2 |
Verma, S. |
PRELIMINARY GUIDELINES ON FLIGHT DECK PROCEDURES FOR VERY CLOSELY SPACED PARALLEL APPROACHES |
ICAS 2008-8.5.2 |
Vermeulen, B. |
AUTOMATING THE DEVELOPMENT PROCESS OF THERMOPLASTIC COMPOSITE SHEET RIBS USING KNOWLEDGE BASED ENG. TECHNIQUES |
ICAS 2008-6.10.3 |
Vernaleken, C. |
SIMULATOR EVALUATION OF A NOVEL SURFACE MOVEMENT AWARENESS AND ALERTING SYSTEM (SMAAS) FOR RUNWAY INCURSION AVOIDANCE |
ICAS 2008-11.11.2 (AIAA 2008-8959) |
Verstraete, D. |
AN ASSESSMENT OF THE POTENTIAL OF HYDROGEN FUELED LARGE LONG-RANGE TRANSPORT AIRCRAFT |
ICAS 2008-1.2.4 |
Verstraete, D. |
PRELIMINARY DESIGN OF A JOINED WING HALE UAV |
ICAS 2008-1.4.3 |
Vesely, L. |
THE EFFECTS OF WALL ROUGHNESS ON THE TURBULENT BOUNDARY LAYER |
ICAS 2008-3.8.1 |
Veul, R. P. G. |
EFFICIENT AEROELASTIC SIMULATION IN A PARAMETRIC PROCEDURE FOR FATIGUE ANALYSIS |
ICAS 2008-7.7.1 |
Vian, J. |
HEALTH MONITORING FOR COMMERCIAL AIRCRAFT SYSTEMS |
ICAS 2008-6.1.2 |
Vieillard, S. |
HIGH EFFICIENCY, HIGH RELIABILITY 2 KW INVERTER FOR AERONAUTICAL APPLICATION |
ICAS 2008-6.1.3 |
Viola, N. |
ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT |
ICAS2008-6.6 ST: |
Visser, H. G. |
OPTIMIZATION OF RNAV NOISE ABATEMENT ARRIVAL TRAJECTORIES |
ICAS 2008-4.11.1 |
Vitic, A. |
PROTOTYPE OF A STIFF WIND TUNNEL BALANCE WITH SEMICONDUCTOR STRAIN GAUGES AND THERMOCOMPENSATION DONE BY SOFTWARE |
ICAS2008-P2.9 |
Viviani, A. |
ANALYSIS OF THERMOCHEMICAL MODELING AND SURFACE CATALYTICITY IN SPACE VEHICLES REENTRY |
ICAS 2008-3.6.2 |
von Kaenel, R. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
Vos, J. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
Vos, R. |
POST-BUCKLED PRECOMPRESSED ELEMENTS: A NEW CLASS OF FLIGHT CONTROL ACTUATORS ENHANCING MORPHING WING UAVS |
ICAS 2008-7.8.2 |
Voskuijl, M. |
CONTROLLABILITY OF BLENDED WING BODY AIRCRAFT |
ICAS 2008-5.4.3 |
Vu, K. -P. L. |
COMPARING SITUATION AWARENESS MEASUREMENT TECHNIQUES IN A LOW FIDELITY AIR TRAFFIC CONTROL SIMULATION |
ICAS 2008-9.7.4 |
Vukovic, D. |
PROTOTYPE OF A STIFF WIND TUNNEL BALANCE WITH SEMICONDUCTOR STRAIN GAUGES AND THERMOCOMPENSATION DONE BY SOFTWARE |
ICAS2008-P2.9 |
Wachendorf, N. |
MULTIVARIABLE CONTROLLER DESIGN FOR A TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WITH TWO PRIMARY LOAD PATHS |
ICAS 2008-6.4.2 |
Wadia, A. |
NUMERICAL INVESTIGATION OF INLET DISTORTION INDUCED SWIRL IN MULTISTAGE FANS |
ICAS 2008-4.4.3 |
Wagner, C. |
SCALING OF MIXED CONVECTION IN AIRCRAFT CABINS |
ICAS 2008-6.3.3 |
Waitz, I. |
ENVIRONMENTAL IMPACT OF AVIATION: A REVIEW OF SELECTED US RESEARCH EFFORTS |
ICAS 2008-0.2 |
Waitz, I. |
INTERDEPENDENCIES IN LOCAL AIR QUALITY AND NOISE IMPACTS FOR LANDING AND TAKEOFF OPERATIONS |
ICAS 2008-11.3.2 (AIAA 2008-8866) |
Wallin, M. |
COMPRESSION STRENGTH OF NOTCHED AND IMPACT DAMAGED COMPOSITE LAMINATES |
ICAS 2008-7.5.2 |
Walther, R. |
CUTTING EDGE TECHNOLOGIES FOR DESIGN, PRODUCTION AND REPAIR OF NEXT GENERATION AERO ENGINES |
ICAS 2008-8.10.2 INVITED |
Wan, F. Y. |
HEALTH MONITORING FOR AEROCRAFT STRUCTURE SYSTEM BY HARMONIC WAVELET TRANSFORM |
ICAS2008-7.7 ST: |
Wan, T. |
NUMERICAL SIMULATION OF FLAPPING WING AERODYNAMIC PERFORMANCE UNDER GUST WIND CONDITIONS |
ICAS2008-3.5 ST: |
Wan, T. |
THE IMPLEMENTATION OF ANALYTICAL HIERARCHY PROCESS IN FLIGHT SAFETY |
ICAS 2008-9.2.4 |
Wang, J. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
Wang, J. A. |
DEVELOPMENT OF FLIGHT CONTROL SYSTEM USING EMBEDDED COMPUTER PC-104 |
ICAS2008-P5.1 |
Wang, J.- G. |
15 THE SIGNAL-TO-NOISE RATIO MODELING OF RADAR IN ELECTRONIC COUNTER-COUNTER MEASURES |
ICAS2008-P6.7 |
Wang, L. |
3 A STUDY ON FATIGUE SCATTER FACTOR OF INDIVIDUAL AIRCRAFT STRUCTURE |
ICAS2008-P3.1 |
Wang, L. |
FATIGUE BEHAVIOR AND LIFE PREDICTION OF WELDED TITANIUM ALLOY JOINTS |
ICAS 2008-7.4.4 |
Wang, S. |
EXTENDING FMC TEST FOR FLIGHT SIMULATION AND FLIGHT EXPERIMENTS |
ICAS 2008-5.5.3 |
Wang, X. |
METHODS FOR CALCULATING THE DAMAGE-RATE OF AIRCRAFT COMPONENT |
ICAS2008-9.8 ST: |
Wang, Y. |
A LAYER PAVEMENT MODEL TO SIMULATE ROUGHNESS FEATURES IN ICE ACCRETION NUMERICAL SIMULATION |
ICAS 2008-2.6.1 |
Wang, Z. |
64 A PROGRAM OF AIRCRAFT EQUIPMENT AND SUBSYSTEMS LIFE EXTENSION |
ICAS2008-P6.1 |
Wang, Z. |
3 A STUDY ON FATIGUE SCATTER FACTOR OF INDIVIDUAL AIRCRAFT STRUCTURE |
ICAS2008-P3.1 |
Wang, Z. |
ANALYSIS OF THE SCATTERING CHARACTERISTICS FROM DISCONTINUITY SURFACES ON AIRCRAFT USING A MODIFIED MLFMA |
ICAS2008-P3.6 |
Wanke, C. |
METHODOLOGIES FOR ESTIMATING THE IMPACT OF SEVERE WEATHER ON AIRSPACE CAPACITY |
ICAS 2008-10.7.4 (AIAA 2008-8917) |
Webb, L. |
KNOWLEDGE MANAGEMENT FOR THROUGH LIFE SUPPORT |
ICAS 2008-6.11.3 |
Weigel, A. L. |
PRELIMINARY ANALYSIS OF STRATEGIES AND CHALLENGES TO ENCOURAGE DATA LINK ADOPTION OVER THE NORTH ATLANTIC AIRSPACE |
ICAS 2008-8.8.3 (AIAA 2008-8953) |
Welch, B. |
AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH |
ICAS 2008-10.3.1 (AIAA 2008-8861) |
Welch, B. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
Wen, X. |
THE APPLICATION OF AIRBORNE VIDEO TECHNOLOGIES DURING AERIAL REFUELING TEST |
ICAS2008-P5.2 |
Westhoff, A. |
SCALING OF MIXED CONVECTION IN AIRCRAFT CABINS |
ICAS 2008-6.3.3 |
Weston, N. |
AN APPROACH FOR MULTI-CRITERIA DECISION MAKING METHOD SELECTION AND DEVELOPMENT |
ICAS 2008-1.3.1 |
Wetzel, A. |
IMPACT RESISTANCE, DAMAGE TOLERANCE AND NON-DESTRUCTIVE DAMAGE DETECTION FOR SANDWICH STRUCTURES: ANALYSIS AND TESTING |
ICAS2008-7.5 ST: |
Wheeler, P. W. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
White, B. A. |
INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT |
ICAS 2008-5.7.3 |
Whitley, C. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
Whitlow Jr., W. |
PROPULSION TECHNOLOGIES FOR THE FUTURE OF AVIATION |
ICAS 2008-8.10.5 INVITED |
Wijekoon, T. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
Wiklund, P. -E. |
VIRTUAL ENTERPRISE COLLABORATION - BREAKTHROUGH TECHNOLOGIES PROVIDED BY VIVACE |
ICAS 2008-8.10.4 INVITED |
Wild, J. |
NUMERICAL AERODYNAMIC OPTIMISATIONS OF 3D HIGH-LIFT CONFIGURATIONS |
ICAS 2008-2.2.3 |
Wildschek, A. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
Wille, T. |
THERMAL ASPECTS FOR COMPOSITE STRUCTURES - FROM MANUFACTURING TO IN-SERVICE PREDICTIONS |
ICAS 2008-7.9.4 |
Willems, B. |
RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY |
ICAS 2008-8.2.3 |
Williams, D. |
INFORMATION REQUIREMENTS FOR SUPERVISORY AIR TRAFFIC CONTROLLERS IN SUPPORT OF A MID-TERM WAKE VORTEX DEPARTURE SYSTEM |
ICAS 2008-8.11.3 |
Williams, D. |
WAKE TURBULENCE MITIGATION FOR ARRIVALS (WTMA) |
ICAS 2008-9.9.3 |
Willis, D. J. |
COMPUTATIONAL INVESTIGATION AND DESIGN OF COMPLIANT MEMBRANE WINGS FOR BIOLOGICALLY INSPIRED FLIGHT VEHICLES |
ICAS 2008-2.10.1 |
Wilson, A. |
NUMERICAL STUDY OF ENERGY UTILIZATION IN NOZZLE/PLUME FLOW-FIELDS OF HIGH-SPEED AIR-BREATHING VEHICLES |
ICAS 2008-4.3.3 |
Winckelmans, G. |
PILOTED SIMULATION RESULTS OF AN ONBOARD WAKE VORTEX DETECTION, WARNING AND AVOIDANCE SYSTEM AND COCKPIT DISPLAY ASPECTS |
ICAS 2008-9.9.1 |
Wing, D. J. |
PERFORMANCE BASIS FOR AIRBORNE SEPARATION |
ICAS 2008-8.7.1 |
Winkler, C. |
A HYBRID, DYNAMIC LARGE EDDY SIMULATION METHOD |
ICAS 2008-2.1.1 |
Wolfe, S. R. |
AN ONTOLOGY FOR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-9.11.1 (AIAA 2008-8946) |
Won, H. T. |
ADVANCED GENERAL AVIATION DESIGN WITH TRANSPORTATION ARCHITECTURE ANALYSIS |
ICAS 2008-1.9.4 (AIAA 2008-8929) |
Wong, H. M. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
Wood, B. |
MICROSCOPIC ANALYSIS OF AIRPORT SURFACE SEQUENCING |
ICAS2008-11.11 ST (AIAA 2008-8961) |
Worden, K. |
A NEGATIVE SELECTION APPROACH TO DETECT DAMAGE IN AERONAUTICAL STRUCTURES WITH CHANGING OPERATING CONDITIONS |
ICAS 2008-9.4.2 |
Wroblewski, W. |
THE INFLUENCE OF FREE - PLAY AND FRICTION IN CONTROL SYSTEM ON AIRCRAFT DYNAMICS |
ICAS 2008-5.10.5 |
Wu, C. |
TERRAIN FOLLOWING FLIGHT REAL-TIME HIL SIMULATION PLATFORM RESEARCH |
ICAS2008-P5.6 |
Wu, D. |
AERODYNAMICS CHARACTERISTICS OF HYPERSONIC VEHICLE IN NEAR SPACE |
ICAS2008-2.5 ST: |
Wu, L. |
STUDY ON THE RELATIONSHIP BETWEEN CORROSION DAMAGE AND RESIDUAL STRENGTH OF AL 7075-T6 ALLOY |
ICAS 2008-9.8.2 |
Wu, X.-R. |
FATIGUE BEHAVIOR AND LIFE PREDICTION OF WELDED TITANIUM ALLOY JOINTS |
ICAS 2008-7.4.4 |
Wu, Z. |
AN UPDATING PROGRAM FOR UNDERGRADUATE AIRCRAFT CONCEPTUAL AND PRELIMINARY DESIGN COURSE |
ICAS2008-P1.5 |
Xia, L. |
THE APPLICATION OF ASEXUAL DNA ALGORITHM TO AIRFOIL DESIGN |
ICAS 2008-2.3.3 |
Xiao, H. |
AERODYNAMICS CHARACTERISTICS OF HYPERSONIC VEHICLE IN NEAR SPACE |
ICAS2008-2.5 ST: |
Xiong, J. T. |
AERODYNAMIC SHAPE OPTIMIZATION OF TRANSONIC AEROELASTIC WING BASED ON CONTROL THEORY |
ICAS2008-9.6 ST: |
Xu, H. |
PREDICTION OF SUPERCOOLED DROPLET IMPINGEMENT ON HELICOPTER ROTOR BLADES |
ICAS 2008-2.6.4 |
Xu, Y. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
Xue, H. J. |
ERGONOMIC ASSESSMENT METHOD FOR COCKPIT LAYOUT OF CIVIL AIRCRAFT X BASED ON VIRTUAL DESIGN |
ICAS2008-P6.5 |
Xue, H. J. |
THE SIMULATION OF THE HUMAN-MACHINE PARTNERSHIP IN UCAV OPERATION |
ICAS 2008-9.10.5 |
Xue, J. |
EFFECTS OF SUSPENSION WEIGHT ON FIGHTER FATIGUE DAMAGE |
ICAS 2008-7.4.5 |
Yadlin, Y. |
FLOW CONTROL TECHNIQUES FOR TRANSPORT AIRCRAFT |
ICAS 2008-3.11.1 |
Yamada, H. |
DEVELOPMENT OF FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT JET ENGINE IN JAXA TECHCLEAN PROJECT |
ICAS 2008-4.3.2 |
Yamamoto, K. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
Yamamoto, K. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
Yamamoto, K. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
Yamamoto, T. |
DEVELOPMENT OF FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT JET ENGINE IN JAXA TECHCLEAN PROJECT |
ICAS 2008-4.3.2 |
Yamashita, H. |
COMPARISON OF SHOCK WAVE INTERACTION FOR THE THREE-DIMENSIONAL SUPERSONIC BIPLANE WITH DIFFERENT PLANAR SHAPES |
ICAS 2008-2.4.5 |
Yamashita, H. |
LOW-BOOM AND LOW-DRAG OPTIMIZATION FOR THE TWIN-ENGINE SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR |
ICAS 2008-2.4.1 |
Yamashita, H. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
Yan, S. W. |
RESEARCH ON FUZZY LOGIC PIO DETECTOR |
ICAS 2008-5.4.5 |
Yan, Y. |
NUMERICAL SIMULATION OF FORMING PROCESS OF AIRCRAFT TRANSPARENCIES MANUFACTURED BY POLYMERIC PLATE |
ICAS2008-P7.1 |
Yanagida, A. |
RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM – PART 1. INTELLIGENT FLIGHT CONTROL SYSTEM |
ICAS 2008-5.10.1 |
Yanagida, A. |
RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM - PART 2 FLIGHT EXPERIMENTS |
ICAS 2008-5.10.2 |
Yang, E. -S. |
DEMAND-CENTRIC ANALYSIS OF THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-10.4.3 (AIAA 2008-8889) |
Yang, W. Q. |
NUMERICAL SIMULATION OF 3D FLAPPING WING BASED ON CHIMERA METHOD |
ICAS 2008-2.10.5 |
Yang, X. D. |
AERODYNAMIC SHAPE OPTIMIZATION OF TRANSONIC AEROELASTIC WING BASED ON CONTROL THEORY |
ICAS2008-9.6 ST: |
Yao, J. |
NUMERICAL INVESTIGATION OF INLET DISTORTION INDUCED SWIRL IN MULTISTAGE FANS |
ICAS 2008-4.4.3 |
Yao, Z. X. |
MISSION DECISION-MAKING METHOD OF MULTI-AIRCRAFT COOPERATIVELY ATTACKING MULTI-TARGET BASED ON SITUATIONAL ASSESSMENT |
ICAS2008-P1.2 |
Yarf-Abbasi, A. |
DESIGN AND DEVELOPMENT OF THE ECLIPSE AND DEMON DEMONSTRATOR UAVS |
ICAS 2008-1.4.2 |
Yashin, Y. |
THEORETICAL APPROACH TO DIRECTIONAL CONTROL SENSITIVITY SELECTION |
ICAS 2008-5.4.1 INVITED |
Yayama, T. |
CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION |
ICAS 2008-1.2.3 |
Ye, K. D. |
IDENTIFYING FATIGUE OF FLIGHT ATTENDANTS IN SHORT-HAUL OPERATIONS |
ICAS 2008-9.2.3 |
Ye, Z. |
NUMERICAL RESEARCHES ON THE AEROELASTIC PROBLEM OF TURBOMACHINERY |
ICAS 2008-4.4.4 |
Yen, J -R. |
IDENTIFYING FATIGUE OF FLIGHT ATTENDANTS IN SHORT-HAUL OPERATIONS |
ICAS 2008-9.2.3 |
Yimer, I. |
DEVELOPMENT OF AN INDUSTRIAL SCALE COMBUSTION TEST AND RESEARCH FACILITY FOR ALTERNATIVE FUELS AND FUEL FLEXIBILITY DEMONSTRATION |
ICAS 2008-4.3.1 |
Yin, Y. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
Yokokawa, Y. |
AEROACOUSTIC NOISE MEASUREMENTS IN AERODYNAMIC LOW-SPEED WIND TUNNELS |
ICAS 2008-3.2.3 |
Yokokawa, Y. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
Yokokawa, Y. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
Yokokawa, Y. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
Yonezawa, M. |
COMPARISON OF SHOCK WAVE INTERACTION FOR THE THREE-DIMENSIONAL SUPERSONIC BIPLANE WITH DIFFERENT PLANAR SHAPES |
ICAS 2008-2.4.5 |
Yonezawa, M. |
LOW-BOOM AND LOW-DRAG OPTIMIZATION FOR THE TWIN-ENGINE SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR |
ICAS 2008-2.4.1 |
Yonezawa, M. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
York, C. B. |
APPROXIMATIONS FOR FULLY ISOTROPIC LAMINATE CONFIGURATIONS |
ICAS 2008-7.3.1 |
Yoshida, K. |
FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1) |
ICAS 2008-2.4.2 |
Young, J. |
FLAPPING-WING TECHNOLOGY: THE POTENTIAL FOR AIR VEHICLE PROPULSION AND AIRBORNE POWER GENERATION |
ICAS 2008-1.5.1 |
Young, T. M. |
SIMPLIFIED METHODS FOR ASSESSING THE IMPACT OF FUEL ENERGY CONTENT ON PAYLOAD-RANGE |
ICAS 2008-11.2.1 (AIAA 2008-8857) |
Yu, T. X. |
HEALTH MONITORING FOR AEROCRAFT STRUCTURE SYSTEM BY HARMONIC WAVELET TRANSFORM |
ICAS2008-7.7 ST: |
Yu, X. |
AN ADAPTABLE METHODOLOGY FOR AUTOMATION APPLICATION DEVELOPMENT |
ICAS 2008-6.2.3 |
Yuan, W. |
A CFD STUDY OF UCAV 1303 BASELINE MODEL AT CRUISE MACH NUMBERS |
ICAS 2008-2.5.1 |
Yun, S. |
DEVELOPMENT OF AN INDUSTRIAL SCALE COMBUSTION TEST AND RESEARCH FACILITY FOR ALTERNATIVE FUELS AND FUEL FLEXIBILITY DEMONSTRATION |
ICAS 2008-4.3.1 |
Zabloudil, M. |
WIND TUNNEL AND COMPUTIONAL INVESTIGATION OF SIMULATED CONTAMINATION ON AIRFOIL |
ICAS2008-P2.11 |
Zaichik, L. |
THEORETICAL APPROACH TO DIRECTIONAL CONTROL SENSITIVITY SELECTION |
ICAS 2008-5.4.1 INVITED |
Zakrzewski, E. |
TERMINAL AREA REQUIRED TIME OF ARRIVAL (RTA) CONCEPT OF OPERATIONS AND AUTOMATION PROTOTYPE |
ICAS 2008-11.9.1 (AIAA 2008-8930) |
Zammit, A. |
BIRD-STRIKE DAMAGE ANALYSIS IN CONCEPT ADVANCED COMPOSITE FAN BLADES |
ICAS 2008-4.4.1 |
Zammit, B. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
Zammit-Mangion, D. |
A RAPID SCENARIO GENERATION TOOL FOR REPEATABLE SIMULATED TRAFFIC CONFLICTS IN FLIGHT SIMULATION |
ICAS 2008-5.1.1 INVITED |
Zammit-Mangion, D. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
Zelinski, S. |
DEFINING DYNAMIC CRITICAL POINTS FOR DYNAMIC AIRSPACE CONFIGURATION |
ICAS 2008-8.9.3 |
Zhan, H. |
THE APPLICATION OF ASEXUAL DNA ALGORITHM TO AIRFOIL DESIGN |
ICAS 2008-2.3.3 |
Zhang, C. |
NUMERICAL RESEARCHES ON THE AEROELASTIC PROBLEM OF TURBOMACHINERY |
ICAS 2008-4.4.4 |
Zhang, D. |
TEST DATA MANAGEMENT FOR AIRCRAFT HYDRAULIC SYSTEM TESTING |
ICAS2008-P6.3 |
Zhang, D. G. |
NUMERICAL SIMULATION OF FORMING PROCESS OF AIRCRAFT TRANSPARENCIES MANUFACTURED BY POLYMERIC PLATE |
ICAS2008-P7.1 |
Zhang, F. |
A CFD STUDY OF UCAV 1303 BASELINE MODEL AT CRUISE MACH NUMBERS |
ICAS 2008-2.5.1 |
Zhang, G. L. |
NUMERICAL SIMULATION OF FORMING PROCESS OF AIRCRAFT TRANSPARENCIES MANUFACTURED BY POLYMERIC PLATE |
ICAS2008-P7.1 |
Zhang, H. |
64 A PROGRAM OF AIRCRAFT EQUIPMENT AND SUBSYSTEMS LIFE EXTENSION |
ICAS2008-P6.1 |
Zhang, J. F. |
275 IMPACT AND COMPRESSION-AFTER-IMPACT PERFORMANCE OF STITCHED/UNSTITCHED COMPOSITE SANDWICH PANELS WITH A FOAM CORE |
ICAS2008-P3.7 |
Zhang, W. |
THE NUMERICAL SIMULATION ANALYSIS OF KEY STRUCTURES OF INTEGRATED POWER SUPPLY IN MOTOR-PUMP |
ICAS2008-P6.2 |
Zhang, Y. F. |
DEVELOPMENT OF FLAPPING WING MICRO AIR VEHICLE |
ICAS 2008-1.5.3 |
Zhang, Y. Z. |
DEVELOPMENT OF FLAPPING WING MICRO AIR VEHICLE |
ICAS 2008-1.5.3 |
Zhao, G. |
THE SYSTEM FAULT BEHAVIOR AND MODEL |
ICAS2008-P9.2 |
Zhao, G. Y. |
THE SYSTEM FAULT BEHAVIOR AND MODEL |
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Zhu, Y. |
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Zurek, J. |
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