DEVELOPMENTS
IN FLIGHT GUIDANCE AND CONTROL , ICAS 2006-0.1: ICAS DANIEL & FLORENCE GUGGENHEIM
MEMORIAL LECTURE: INVITED: |
General Lecture |
THE A380 PROGRAMME, ICAS 2006-0.6: VON KARMAN LECTURE: INVITED:
(approved draft) |
General Lecture |
DESIGN OF THE BLENDED-WING-BODY
SUBSONIC TRANSPORT , ICAS 2006-0.7: LUDWIG BÖLKOW LECTURE: |
General Lecture |
DISTRIBUTED ON-DEMAND AIR TRANSPORTATION
USING SMALL AIRPLANES AND SMALL AND UNDERUTILIZED COMMUNITY AIRPORTS
, ICAS 2006-0.5: GENERAL LECTURE IV: INVITED: |
General Lecture |
KEY TECHNOLOGY ENABLERS FOR THE
FUTURE OF AERONAUTICAL EQUIPMENT INDUSTRY , ICAS 2006-0.2: GENERAL LECTURE
I: INVITED: |
General Lecture |
THE EDUCATION OF FUTURE AERONAUTICAL
ENGINEERS: CONCEIVING, DESIGNING, IMPLEMENTING AND OPERATING ,
ICAS 2006-0.4: GENERAL LECTURE III: INVITED: |
General Lecture |
THE INTERNATIONAL DEVELOPMENT
AND PRODUCTION OF THE F2-FIGHTER , ICAS 2006-0.3: GENERAL LECTURE
II: INVITED: |
General Lecture |
A BRAZILIAN
EXPERIENCE IN TEACHING AIRCRAFT DESIGN , ICAS 2006-P1.4 |
1. Aircraft and Systems Integration |
A COMPARATIVE STUDY OF FOUR UCAV
WING LAYOUTS - HIGH SPEED AERO PERFORMANCE & STABILITY CONSIDERATIONS
, ICAS 2006-1.7.2 |
1. Aircraft and Systems Integration |
A COMPARISON OF EMPIRICAL AND
CFD-BASED EXERGY MODELLING FOR THE AIRFRAME SUBSYSTEM OF AIRCRAFT
DESIGN , ICAS 2006-1.9.2 |
1. Aircraft and Systems Integration |
A HYBRID GENETIC/LNTERIOR-POINT
ALGORITHM FOR MULTI-DISCIPLINARY OPTIMIZATION PROBLEMS IN AIRCRAFT
PRELIMINARY DESIGN, ICAS 2006-1.11.1 |
1. Aircraft and Systems Integration |
A METHODOLOGY FOR TECHNOLOGY
EVALUATION AND CAPABILITY TRADEOFF FOR COMPLEX SYSTEM ARCHITECTURES
, ICAS 2006-1.2.1 |
1. Aircraft and Systems Integration |
A MORPHING UAV WITH ROTARY AND
FIXED-WING MODES , ICAS 2006-1.10.5 |
1. Aircraft and Systems Integration |
A NEW METHOD FOR OPTIMUM ALLOCATION
OF DESIGN REQUIREMENTS IN AIRCRAFT CONCEPTUAL DESIGN , ICAS2006-1.11S |
1. Aircraft and Systems Integration |
A POWERED LIFT DESIGN FOR SUBSONIC
CIVIL TRANSPORT AIRCRAFT , ICAS2006-1.3S |
1. Aircraft and Systems Integration |
A PRACTICAL MULTIDISCIPLINARY
DESIGN OPTIMIZATION ALGORITHM BASED ON THE UNIFORM DESIGN THEORY , ICAS2006-1.9S |
1. Aircraft and Systems Integration |
A VIRTUAL ENVIRONMENT, DISTRIBUTED
SIMULATION, UAV TESTBED , ICAS2006-1.10S |
1. Aircraft and Systems Integration |
AERODYNAMIC PERFORMANCE OF A
BLENDED-WING-BODY CONFIGURATION AIRCRAFT , ICAS 2006-1.6.2 |
1. Aircraft and Systems Integration |
AN ENHANCED SCENARIO APPROACH
ASSESSING UNCERTAINTIES IN THE REALIZATION OF NEW AIRCRAFT AND TECHNOLOGIES
, ICAS 2006-1.9.1 |
1. Aircraft and Systems Integration |
AN INTEGRATED AND GENERIC VULNERABILITY
ASSESSMENT SYSTEM FOR AIRCRAFT NONNUCLEAR SURVIVABILITY DESIGN , ICAS 2006-1.2.4 |
1. Aircraft and Systems Integration |
AN INTEGRATED PLATFORM FOR AIRCRAFT
DESIGN: FLIGHT ENGINEERING SIMULATOR , ICAS 2006-P1.1 |
1. Aircraft and Systems Integration |
AN INTEGRATED SYSTEM FOR BORDER
SURVEILLANCE AND MONITORING BASED ON VERY LIGHT MALE UAV , ICAS 2006-1.7.5 |
1. Aircraft and Systems Integration |
AN INTELLIGENT, KNOWLEDGE-BASED
MULTI-CRITERIA DECISION MAKING ADVISOR FOR AEROSPACE SYSTEMS DESIGN
, ICAS 2006-1.9.3 |
1. Aircraft and Systems Integration |
AN OVERVIEW OF AIRCRAFT MECHANICS
AND STRUCTURES , ICAS 2006-1.5.1 |
1. Aircraft and Systems Integration |
APPLICATION OF THE VARIABLE-FIDELITY
MDO TOOLS TO A JET AIRCRAFT DESIGN , ICAS 2006-1.8.1 |
1. Aircraft and Systems Integration |
AUTOMATION OF CONCEPTUAL DESIGN
OF VERTICAL TAKE-OFF UAVS – DEMONSTRATION MODEL , ICAS 2006-1.10.1 |
1. Aircraft and Systems Integration |
CONCEPTUAL DESIGN OF ROADABLE
AIRCRAFT , ICAS 2006-1.4.5 |
1. Aircraft and Systems Integration |
DESIGN AND TESTING OF A MODEL
WING SECTION FOR A HUMAN POWERED AIRCRAFT , ICAS 2006-P1.2 |
1. Aircraft and Systems Integration |
DESIGN APPROACH FOR A VERTICAL
TAKE-OFF UNMANNED AERIAL VEHICLE WITH INTEROPERABLE CAPABILITIES –
PAYLOAD ISSUES , ICAS2006-1.10S |
1. Aircraft and Systems Integration |
DESIGN TRENDS FOR ROTARY-WING
UNMANNED AIR VEHICLES , ICAS 2006-1.10.2 |
1. Aircraft and Systems Integration |
DESIGN, ANALYSIS, FABRICATION
AND FLIGHT TEST VALIDATION OF THE NWPU25 MICRO AIR VEHICLE ,
ICAS 2006-1.10.3 |
1. Aircraft and Systems Integration |
DEVELOPMENT AND FLIGHT TESTING
OF AN AUTONOMOUS PARAFOIL-LOAD SYSTEM DEMONSTRATOR , ICAS 2006-1.1.3 |
1. Aircraft and Systems Integration |
DEVELOPMENT OF AN MAV MANEUVERED
BY SHIFTING THE LOCATION OF CENTER OF GRAVITY , ICAS 2006-1.10.4 |
1. Aircraft and Systems Integration |
DEVELOPMENT OF EXPERIMENTAL SMALL
UAV EQUIPPED WITH CELLULAR PHONE DATA LINK SYSTEM ,
ICAS2006-1.7S |
1. Aircraft and Systems Integration |
DISTRIBUTED PROPULSION FEASIBILITY
STUDIES , ICAS 2006-1.3.2 |
1. Aircraft and Systems Integration |
EDUCATIONAL FLIGHT TESTING, ICAS 2006-1.5.2 |
1. Aircraft and Systems Integration |
ELECTRIC POWERED COMMUTER AIRCRAFT, ICAS2006-1.6S |
1. Aircraft and Systems Integration |
EUROPEAN ACTIVITIES FOR CIVIL
UAV APPLICATIONS , ICAS 2006-1.7.1 |
1. Aircraft and Systems Integration |
EVOLUTIONAL DESIGN SUPPORT STRATEGY
ORIENTED TO AIRCRAFT CONCEPTUAL DESIGN , ICAS2006-1.2S |
1. Aircraft and Systems Integration |
FIRST RESULTS OF THE 2ND FLIGHT TEST CAMPAIGN USING
AN AIRBUS A 340 IN THE EUROPEAN AWIATOR PROJECT ON WING TECHNOLOGIES, ICAS 2006-1.3.1 |
1. Aircraft and Systems Integration |
FITTING FITNESS IN AIRCRAFT DESIGN
, ICAS 2006-1.11.3 |
1. Aircraft and Systems Integration |
FLAVIIR, AN INNOVATIVE UNIVERSITY
/ INDUSTRY RESEARCH PROGRAM FOR COLLABORATIVE RESEARCH & DEMONSTRATION
OF UAV TECHNOLOGIES , ICAS 2006-1.1.2 |
1. Aircraft and Systems Integration |
HYDROGEN FUELLED LARGE LONG RANGE TRANSPORT AIRCRAFT, ICAS 2006-1.4.3 |
1. Aircraft and Systems Integration |
INTEGRATION OF DESIGN TO SUPPORT
AS PART OF AIRCRAFT DEVELOPMENT , ICAS 2006-1.8.3 |
1. Aircraft and Systems Integration |
LOCAL PARETO ANALYSER FOR PRELIMINARY
DESIGN , ICAS 2006-1.11.2 |
1. Aircraft and Systems Integration |
LOW COST, FLEXIBLE PLATFORM FOR
IN SITU REMOTE SENSING , ICAS 2006-1.1.1 |
1. Aircraft and Systems Integration |
MULTIOBJECTIVE OPTIMIZATION OF ENGINE & A/C MATCHING
ON MISSION AND ENVIRONMENTAL CRITERIA AT SSBJ CONCEPTUAL DESIGN, ICAS2006-1.4S |
1. Aircraft and Systems Integration |
MULTIOBJECTIVE EVOLUTIONARY ALGORITHMS
APPLIED TO AIRCRAFT ENGINE DESIGN , ICAS 2006-1.8.2 |
1. Aircraft and Systems Integration |
National Experimental Supersonic
Transport Project , ICAS 2006-1.4.1 INVITED: |
1. Aircraft and Systems Integration |
NOVEL CONCEPTS FOR AIRCRAFT COMPONENT TECHNOLOGIES:
THE NACRE EUROPEAN INTEGRATED PROJECT, ICAS 2006-1.6.1 |
1. Aircraft and Systems Integration |
ON THE DESIGN OPTIMIZATION OF A THRUST-VECTORED HIGH-SUBSONIC
JET TRANSPORT AIRCRAFT, ICAS2006-1.4S |
1. Aircraft and Systems Integration |
OPTIMISING TRANSPORT FLYING WINGS
, ICAS 2006-1.6.3 |
1. Aircraft and Systems Integration |
PRELIMINARY DESIGN OF A RANGE OF HYDROGEN-POWERED CIVIL
TRANSPORT AIRCRAFT, ICAS 2006-1.4.4 |
1. Aircraft and Systems Integration |
PULSED PLASMA PROPULSION AND FLOW CONTROL FOR BIONIC
AIRSHIPS,
ICAS2006-1.6S |
1. Aircraft and Systems Integration |
RE-ANALYSIS OF A MULTI-MISSION
RE-CONFIGURABLE UAV – REVISED DESIGN CONCEPT , ICAS 2006-1.7.4 |
1. Aircraft and Systems Integration |
REPETITIVE RESPONSE SURFACE ENHANCEMENT TECHNIQUE THROUGH
DESIGN SPACE TRANSFORMATION AND SUB-OPTIMIZATION, ICAS2006-1.9S |
1. Aircraft and Systems Integration |
REPRESENTATION OF STRUCTURAL
SOLUTIONS IN BLENDED WING BODY PRELIMINARY DESIGN , ICAS 2006-1.6.4 |
1. Aircraft and Systems Integration |
SILENT SUPERSONIC TECHNOLOGY
DEMONSTRATION PROGRAM , ICAS 2006-1.4.2 |
1. Aircraft and Systems Integration |
STUDY ON DECISION CONFLICT OF
UAV SYSTEM , ICAS 2006-P1.3 |
1. Aircraft and Systems Integration |
STUDY ON DESIGN AND TRANSITIONAL
FLIGHT OF TAIL-SITTING VTOL UAV , ICAS 2006-1.7.3 |
1. Aircraft and Systems Integration |
SURVIVABILITY EVALUATION AND
SUSTAINABLE DEVELOPABILITY INTEGRATED TRADEOFF METHODS FOR MILITARY
AIRCRAFT , ICAS 2006-1.2.2 |
1. Aircraft and Systems Integration |
THE DESIGN OF A HIGH-MANEUVERABLE SINGLE- MINI-JET ENGINED
REMOTELY PILOTED VEHICLE (RPV), ICAS2006-1.1S |
1. Aircraft and Systems Integration |
THE INVESTIGATION OF CYCLOGYRO
DESIGN AND THE PERFORMANCE , ICAS 2006-1.3.3 |
1. Aircraft and Systems Integration |
THE RESEARCH OF STRUCTURAL OPTIMIZATION
WITH THE CONSTRAINTS OF AERODYNAMICS AND RADAR CROSS SECTION (RCS)
OF AIRCRAFT , ICAS 2006-1.9.4 |
1. Aircraft and Systems Integration |
TRANSPORT AIRCRAFT RESEARCH CHALLENGES
– DLR-ONERA PARTNERSHIP , ICAS 2006-1.3.4 |
1. Aircraft and Systems Integration |
USING INFORMATION ENTROPY TO
ASSESS AIRCRAFT SIGNATURES INTEGRATED EFFECT , ICAS 2006-1.2.3 |
1. Aircraft and Systems Integration |
A BEST PRACTICES
SYSTEM FOR REDUCED UNCERTAINTY IN CFD , ICAS 2006-2.6.1 |
2. Aerodynamics |
A CFD ANALYSIS OF THE 14-BIS
AIRCRAFT AERODYNAMICS , ICAS 2006-2.2.2 |
2. Aerodynamics |
A COUPLED PRESCRIBED WAKE-EULER
SOLVER FOR EFFICIENT COMPUTING HELICOPTER ROTOR FLOWS IN HOVER ,
ICAS 2006-2.2.4 |
2. Aerodynamics |
A NEW APPROACH IN CFD SUPPORTED
WIND TUNNEL TESTING , ICAS 2006-3.4.2 |
2. Aerodynamics |
A STUDY OF NONLINEAR EDDY-VISCOSITY
MODELS IN A FLOW SOLVER FOR TURBOMACHINERY , ICAS 2006-2.5.2 |
2. Aerodynamics |
A STUDY ON AERODYNAMIC DESIGN
INTEGRATION OF THE SUPERCRITICAL WING AND REAR-MOUNTED ENGINE CONFIGURATION
, ICAS 2006-P2.5 |
2. Aerodynamics |
A VARIABLE FIDELITY OPTIMIZATION
FRAMEWORK USING SECOND-ORDER, MULTI-POINT, ADDITIVE SCALING FUNCTIONS
APPLIED TO AIRFOIL DESIGN , ICAS 2006-P2.17 |
2. Aerodynamics |
ACTIVE CONTROL OF SEPARATION
ON TWO AND THREE DIMENSIONAL HIGH-LIFT CONFIGURATIONS , ICAS 2006-3.5.1 |
2. Aerodynamics |
ADAPTIVE LOAD REDISTRIBUTION
USING MINI-TEDS , ICAS 2006-3.9.1 |
2. Aerodynamics |
AERODYNAMIC COEFFICIENT PREDICTION
OF A GENERAL TRANSPORT AIRCRAFT USING NEURAL NETWORK , ICAS 2006-2.6.3 |
2. Aerodynamics |
AERODYNAMIC DESIGN FOR WING-BODY
BLENDED AND INLET , ICAS 2006-P2.16 |
2. Aerodynamics |
AERODYNAMIC EFFICIENCY STUDY
OF MODERN SPIROID WINGLETS , ICAS2006-3.7S |
2. Aerodynamics |
AERODYNAMIC MODELING USING FLIGHT
MECHANICAL SIMULATIONS, FLIGHT TESTS AND OPTIMIZATION , ICAS 2006-3.10.3 |
2. Aerodynamics |
AERODYNAMIC SHAPE OPTIMIZATION
OF TRANSONIC AIRFOIL AND WING USING RESPONSE SURFACE METHODOLOGY ,
ICAS 2006-2.1.3 |
2. Aerodynamics |
AERODYNAMIC SHAPE OPTIMIZATION
OF UNGUIDED PROJECTILES USING ANT COLONY OPTIMIZATION AND GENETIC
ALGORITHM , ICAS2006-3.6S |
2. Aerodynamics |
AERODYNAMIC STUDY OF A BLENDED
WING BODY; COMPARISON WITH A CONVENTIONAL TRANSPORT AIRPLANE ,
ICAS 2006-P2.8 |
2. Aerodynamics |
AERODYNAMIC STUDY OF HIGH-LIFT
DEVICE CONFIGURATIONS FOR TAKE-OFF AND LANDING CONDITIONS , ICAS 2006-2.3.2 |
2. Aerodynamics |
AEROLOADS. A TOOL TO GENERATE PRESSURE LOAD MODELS OF
AN AIRCRAFT FITTED TO AN AERODYNAMIC DATA BASE, ICAS2006-3.9S |
2. Aerodynamics |
AIAA CFD DRAG PREDICTION WORKSHOP:
AN OVERVIEW , ICAS 2006-2.4.1 |
2. Aerodynamics |
AIRBRAKE INDUCED FIN BUFFET LOADS
ON FIGHTER AIRCRAFT , ICAS 2006-3.9.2 |
2. Aerodynamics |
AIRFOIL DESIGN OF TAILLESS UNMANNED
AIR VEHICLE (UAV) , ICAS 2006-P2.7 |
2. Aerodynamics |
AN EFFICIENT PRECONDITIONING
METHOD AND ITS APPLICATION TO NUMERICAL SIMULATION OF STEADY AND UNSTEADY
VISCOUS FLOWS , ICAS 2006-2.6.4 |
2. Aerodynamics |
AN EXPERIMENTAL AND ANALYTICAL
INVESTIGATION OF AERODYNAMIC FLOW CONTROL USING SYNTHETIC JET TECHNOLOGY
, ICAS 2006-P2.3 |
2. Aerodynamics |
ANALYTICAL SOLUTION OF THE EULER
EQUATIONS FOR AIRFOIL FLOW AT SUBSONIC AND TRANSONIC CONDITIONS ,
ICAS 2006-2.4.4 |
2. Aerodynamics |
ANGLE-OF-ATTACK IMPACT ON THE
AEROTHERMODYNAMIC PERFORMANCE OF FLAT-NOSE POWER-LAW BODIES IN HYPERSONIC
AIRFLOW , ICAS 2006-2.7.3 |
2. Aerodynamics |
APPLICATION OF ADVANCED SURFACE
SENSORS FOR THE DETECTION AND CONTROL OF FLOW SEPARATION ON AN INDUSTRIAL
HIGH-LIFT CONFIGURATION , ICAS 2006-2.11.3 |
2. Aerodynamics |
APPLICATIONS OF DIFFERENT MEASURING
TECHNIQUES FOR TRANSITION DETECTION IN LOW AND HIGH SPEED FLIGHT EXPERIMENTS
, ICAS 2006-3.3.1 |
2. Aerodynamics |
BOUNDARY-LAYER CONTROL BY BLOWING
AT THE TEST-SECTION OF A LOW-SPEED WIND TUNNEL , ICAS 2006-3.4.3 |
2. Aerodynamics |
COMPUTATION OF EQUIVALENT ACOUSTIC SOURCES USING AN
INVERSE METHOD, ICAS 2006-P2.23 |
2. Aerodynamics |
COMPUTATIONAL ANALYSES OF SUPERSONIC
FLOWS OVER A DELTA WING AT HIGH ANGLES OF ATTACK , ICAS2006-2.5S |
2. Aerodynamics |
COMPUTATIONAL INVESTIGATION OF THE FLIR POD INTERFERENCE
EFFECTS ON THE CF-18 AIRCRAFT STORES, ICAS 2006-2.2.1 |
2. Aerodynamics |
COMPUTATIONAL AEROACOUSTIC PREDICTION
OF TRANSONIC ROTOR NOISE BASED ON REYNOLDS-AVERAGED N-S FLOW SIMULATION
, ICAS 2006-2.10.3 |
2. Aerodynamics |
COMPUTATIONAL AERODYNAMIC ANALYSIS
ON A GENERIC UCAV/URAV CONFIGURATION , ICAS2006-2.2S |
2. Aerodynamics |
COMPUTATIONAL AERODYNAMIC BEHAVIOUR
OF LOCATION AND INCLINATION OF LATERAL PLATE /JET- INTERACTIONS
WITH HYPERSONIC FLOWFIELD , ICAS2006-2.7S |
2. Aerodynamics |
CONIC CURVE DESCRIPTION OF FLAPPING WING PLANFORMS AND
PARAMETRIC INVESTIGATION OF THEIR PERFORMANCE, ICAS2006-3.10S |
2. Aerodynamics |
COST-EFFICIENT USE OF PARALLEL
COMPUTERS IN AIRCRAFT DESIGN , ICAS 2006-2.6.2 |
2. Aerodynamics |
DECAY CHARACTERISTICS OF SINGLE
AND DOUBLE WAKE-VORTEX PAIRS IN DIFFERENT ATMOSPHERIC FLOW REALISATIONS
, ICAS 2006-3.8.1 |
2. Aerodynamics |
DESIGN FOR SPIN ,
ICAS 2006-3.11.2 |
2. Aerodynamics |
DEVELOPMENT OF A NEW BOUNDARY
LAYER CONTROL TECHNIQUE FOR AUTOMOTIVE WIND TUNNEL TESTING ,
ICAS 2006-3.5.3 |
2. Aerodynamics |
DIRECT MEASUREMENT OF WALL-SHEAR
STRESS OF PLANE SHEAR LAYER WITH PLASMA SYNTHETIC JET ACTUATOR ,
ICAS2006-3.5S |
2. Aerodynamics |
DNW’S METHOD TO CORRECT FOR SUPPORT
AND WALL INTERFERENCE EFFECTS ON LOW SPEED MEASUREMENTS WITH A LARGE
PROPELLER POWERED TRANSPORT AIRCRAFT MODEL , ICAS 2006-3.4.5 |
2. Aerodynamics |
DUAL-CODE SOLUTION PROCEDURE
FOR EQUILIBRIUM HYPERSONIC AXISYMMETRIC TRANSITIONAL/TURBULENT FLOWS
, ICAS 2006-2.4.5 |
2. Aerodynamics |
EFFECT OF CENTER-BODY ON THE
VORTEX FLOW OF A DELTA WING WITH LEADING EDGE EXTENSION , ICAS 2006-3.1.1 |
2. Aerodynamics |
EFFECTS OF HELICOPTER ROTOR WAKE
CHARACTERISTICS ON BLADE AIRLOADS , ICAS 2006-3.8.3 |
2. Aerodynamics |
EULERIAN WATER IMPINGEMENT PREDICTION ON MULTI-ELEMENT
AIRFOILS WITH VISCOUS AND INVISCID FLOW, ICAS2006-2.5S |
2. Aerodynamics |
EXERGY BASED DESIGN METHODOLOGY
FOR AIRFOIL SHAPE OPTIMIZATION AND WING ANALYSIS , ICAS2006-3.11S |
2. Aerodynamics |
EXPERIMENTAL AND NUMERICAL ANALYSIS
ON LIFT AND TRANSITION CHARACTERISTICS OF ONERA-M5 CONFIGURATION MODEL
, ICAS 2006-2.3.3 |
2. Aerodynamics |
EXPERIMENTAL AND NUMERICAL STUDY
OF A TWO-ELEMENT WING WITH GURNEY FLAP , ICAS2006-3.8S |
2. Aerodynamics |
EXPERIMENTAL RESEARCH OF AERODYNAMICS
ON AN SST CONFIGURATION WITH HIGH LIFT DEVICES , ICAS 2006-5.11.3 |
2. Aerodynamics |
EXPERIMENTAL STUDY AND NUMERICAL
SIMULATION OF FLOW AROUND WING CONTROL SURFACE , ICAS 2006-3.6.2 |
2. Aerodynamics |
EXPERIMENTAL STUDY OF CONTAMINATED
AIRFOIL WITH FOWLER FLAP , ICAS2006-3.5S |
2. Aerodynamics |
FLAPPING-WING THRUST IN COMPRESSIBLE
FLOW , ICAS 2006-3.10.4 |
2. Aerodynamics |
FLOW SIMULATION OF AN SST CONFIGURATION
AT LOW-SPEED AND HIGH-LIFT CONDITIONS , ICAS 2006-3.7.3 |
2. Aerodynamics |
FORCED HEAVE OSCILLATIONS OF A SUPERCRITICAL SWEPT WING
IN TRANSONIC FLOW, ICAS 2006-3.2.3 |
2. Aerodynamics |
GEOMETRY MODIFICATIONS OF NONPLANAR
WING TIP DESIGN FOR ADAPTATION TO LOW SPEED RANGE , ICAS 2006-3.11.3 |
2. Aerodynamics |
GROUND MOBILE LABORATORY FOR
MEASUREMENT OF AIRFOIL AERODYNAMIC CHARACTERISTICS , ICAS2006-3.4S |
2. Aerodynamics |
HALF MODEL TESTING AND SIDEWALL
EFFECTS , ICAS2006-3.4S |
2. Aerodynamics |
HEAT TRANSFER CHARACTERISTICS
OF LITHIUM COOLANT FLOWING THROUGH A CURVED BEND USING MODIFIED TOROIDAL
COORDINATE SYSTEM , ICAS 2006-P2.15 |
2. Aerodynamics |
HICON AERODYNAMICS- HIGH LIFT
AERODYNAMIC DESIGN FOR THE FUTURE , ICAS 2006-3.7.5 |
2. Aerodynamics |
IHAAA APPLICATIONS TO STORE SEPARATION
, ICAS 2006-P2.9 |
2. Aerodynamics |
IMPACT OF MODEL PLUNGING MOTION
ON WIND TUNNEL WALL PRESSURE FLUCTUATIONS , ICAS2006-3.2S |
2. Aerodynamics |
IMPLEMENTATION OF HIGH-ORDER
COMPACT SCHEMES TO THE ITERATIVE PARABOLIZED NAVIER-STOKES EQUATIONS
, ICAS 2006-2.1.2 |
2. Aerodynamics |
INCOMPRESSIBLE NAVIER STOKES
EQUATIONS SOLUTION USING BLOCK NESTED CARTESIAN GRID , ICAS2006-2.1S |
2. Aerodynamics |
INFLUENCE OF CAPTIVE STORES ON
THE UNSTEADY PRESSURE DISTRIBUTION WITHIN A RECTANGULAR CAVITY ,
ICAS 2006-3.9.4 |
2. Aerodynamics |
INITIAL STEADY / UNSTEADY CFD
ANALYSIS OF VORTEX FLOW OVER THE VFE-2 DELTA WING , ICAS 2006-P2.18 |
2. Aerodynamics |
INVESTIGATING ACTIVE VORTEX GENERATORS
AS A NOVEL HIGH-LIFT DEVICE , ICAS 2006-3.7.4 |
2. Aerodynamics |
INVESTIGATION OF ERROR SOURCES
ON THE BALANCE AND THE STANDARD DYNAMIC MODEL IN THE WIND TUNNEL ,
ICAS2006-3.2S |
2. Aerodynamics |
INVESTIGATION OF FLOW PHENOMENA
ON GENERIC DELTA WING , ICAS 2006-3.1.2 |
2. Aerodynamics |
INVESTIGATION ON AN ACTIVE WINGLET
INFLUENCING THE WAKE OF A LARGE TRANSPORT AIRCRAFT , ICAS 2006-3.8.2 |
2. Aerodynamics |
INVESTIGATIONS OF UNSTEADY FLOW FIELDS IN TRANSONIC
WIND TUNNELS USING PARTICLE IMAGE VELOCIMETRY, ICAS 2006-3.2.4 |
2. Aerodynamics |
LAMINAR AIRFOIL MODIFICATION
ATTAINING OPTIMUM DRAG REDUCTION BY USE OF AIRFOIL MORPHING ,
ICAS 2006-2.7.1 |
2. Aerodynamics |
LAMINAR-TURBULENT TRANSITION
CORRELATIONS IN SUPERSONIC/ HYPERSONIC FLOW , ICAS 2006-3.6.4 |
2. Aerodynamics |
MODELING AND CONTROL OF A WIRE-DRIVEN
PARALLEL SUPPORT SYSTEM WITH LARGE ATTACK ANGLES IN LOW SPEED WIND
TUNNELS , ICAS 2006-3.5.2 |
2. Aerodynamics |
MODELLING OF DYNAMIC STABILITY
DERIVATIVES USING CFD , ICAS 2006-3.10.5 |
2. Aerodynamics |
MODIFICATION OF DELTA WINGS TO CONTROL VORTEX BREAKDOWN,
ICAS 2006-P2.19 |
2. Aerodynamics |
MULTIBODY SIMULATION OF AN AEROELASTIC DELTA WING IN
ROLL MANOEUVRES, ICAS 2006-3.10.2 |
2. Aerodynamics |
NEW MEASUREMENT TECHNIQUES IN
THE ONERA LARGE WIND TUNNELS , ICAS 2006-3.3.3 |
2. Aerodynamics |
NOISE GENERATION AROUND NACA0012
WINGTIP USING LARGE-EDDY-SIMULATION , ICAS 2006-2.10.1 |
2. Aerodynamics |
NON-LINEAR PHENOMENA ANALYSIS
AND CHAOS PREDICTION OF STALL-INDUCED AEROELASTIC OSCILLATIONS VIA
LYAPUNOV EXPONENTS , ICAS2006-3.10S |
2. Aerodynamics |
NUM. AND EXP. INVESTIGATIONS ON THE APPLICATION OF VORTEX
GENERATORS FOR SHOCK WAVE-/BOUNDARY LAYER-INTERACTION CONTROL, ICAS 2006-2.9.3 |
2. Aerodynamics |
NUMERICAL ANALYSIS OF FLAPPING
WING , ICAS 2006-2.2.3 |
2. Aerodynamics |
NUMERICAL CALCULATION OF CONFINED
COAXIAL TURBULENT SWIRLING JETS , ICAS 2006-P2.1 |
2. Aerodynamics |
NUMERICAL COMPUTATION OF THE
X-15 WIND TUNNEL AND FLIGHT EXPERIMENTS: A VALIDATION AND VERIFICATION
CASE STUDY , ICAS 2006-2.4.3 |
2. Aerodynamics |
NUMERICAL DESIGN AND ASSESSMENT
OF A BIPLANE AS FUTURE SUPERSONIC TRANSPORT- REVISITING BUSEMANN'S
BIPLANE , ICAS 2006-3.7.2 |
2. Aerodynamics |
NUMERICAL INVESTIGATION ON THE
AERODYNAMIC EFFECT OF MINI-TEDS ON THE AWIATOR AIRCRAFT CONFIGURATION
AT CRUISE CONDITIONS , ICAS 2006-3.9.3 |
2. Aerodynamics |
NUMERICAL SIMULATION OF COMPLEX
ICE SHAPES ON SWEPT WINGS , ICAS 2006-2.5.1 |
2. Aerodynamics |
NUMERICAL SIMULATION OF KINETIC
EFFECTS IN LOW-DENSITY HYPERSONIC AERODYNAMICS , ICAS 2006-P2.4 |
2. Aerodynamics |
NUMERICAL SIMULATION OF THE FLOWFIELD
AROUND MISSILE WITH LATERAL JET INTERACTION , ICAS2006-2.2S |
2. Aerodynamics |
NUMERICAL SIMULATION OF THIN
AIRFOIL STALL BY USING MODIFIED DES APPROACH , ICAS 2006-2.5.3 |
2. Aerodynamics |
NUMERICAL STUDY OF FLOWS IN THE
VICINITY OF AIRFOIL TRAILING EDGE , ICAS 2006-2.10.2 |
2. Aerodynamics |
NUMERICAL STUDY OF THE PERFORMACE
IMPROVEMENT OF SUBMERGED AIR INTAKES USING VORTEX GENERATORS ,
ICAS 2006-P2.12 |
2. Aerodynamics |
NUMERICAL STUDY OF EFFECTS OF
INJECTION PRESSURE AND LOCATION OF SECONDARY INJECTION INSIDE LOW-THRUST
SATELLITE NOZZLE , ICAS 2006-P2.10 |
2. Aerodynamics |
ON IMPROVING STABILITY AND EFFICIENCY
OF LU-SGS METHOD FOR INCOMPRESSIBLE VISCOUS FLOWS WITH PSEUDO COMPRESSIBILITY
, ICAS 2006-2.1.1 |
2. Aerodynamics |
ON STATUS OF WIND TUNNEL WALL
CORRECTION , ICAS 2006-3.4.4 |
2. Aerodynamics |
ON THE CORRELATION OF ACOUSTIC
MODES IN A NOZZLE AND IN THE FAR-FIELD , ICAS 2006-2.10.4 |
2. Aerodynamics |
ONE-SHOT PSEUDO-TIMESTEPPING METHOD FOR AERODYNAMIC
SHAPE OPTIMIZATION, ICAS2006-2.6S |
2. Aerodynamics |
ONGOING ACTIVITIES IN FLOW SIMULATION
AND SHAPE OPTIMIZATION WITHIN THE GERMAN MEGADESIGN PROJECT ,
ICAS 2006-3.11.1 |
2. Aerodynamics |
OPTIMIZATION OF THE AFT-BODY
GEOMETRY OF AXI-SYMMETRIC SLENDER BODY BASED ON WAVE DRAG CONSIDERATIONS
, ICAS 2006-3.6.3 |
2. Aerodynamics |
Performance Testing with High
Productivity in a Low Speed Flight Reynolds Number Test Campaign ,
ICAS 2006-5.11.1 |
2. Aerodynamics |
PIV INVESTIGATION OF AN AIRFOIL
WITH A GURNEY FLAP , ICAS 2006-3.1.3 |
2. Aerodynamics |
PIV STUDY OF NEAR WALL ORGANIZED
MOTIONS , ICAS 2006-P2.22 |
2. Aerodynamics |
PREDICTION OF HIGH-LIFT SYSTEM AERODYNAMICS USING UNSTRUCTURED-GRID
FLOW SOLVERS AND TRANSPORT EQUATION TURBULENCE MODEL, ICAS2006-2.3S |
2. Aerodynamics |
PREDICTION OF AERODYNAMICS CHARACTERISTICS
AND AIRLOADS OF A GENERIC GEOMETRY WING. ,
ICAS 2006-P2.14 |
2. Aerodynamics |
PRELIMINARY EXPERIMENTS OF FLAPPING
WING IN THREE-DEGREE-OF-FREEDOM MOTIONS , ICAS 2006-3.2.2 |
2. Aerodynamics |
PROPULSIVE CHARACTERISTICS OF
BIOMORPHING AIRFOILS IN GROUND EFFECT , ICAS2006-2.7S |
2. Aerodynamics |
RECENT EFFORTS FOR CREDIBLE CFD
SIMULATIONS IN CHINA , ICAS 2006-2.4.2 |
2. Aerodynamics |
REYNOLDS NUMBER EFFECTS IDENTIFIED
WITH CFD METHODS COMPARED TO SEMI-EMPIRICAL METHODS , ICAS 2006-2.3.4 |
2. Aerodynamics |
ROBUST AIRFOIL OPTIMIZATION BASED ON RESPONSE SURFACE
METHOD (RSM), ICAS 2006-P2.6 |
2. Aerodynamics |
SEMI-SPAN TESTING IN WIND TUNNELS
, ICAS 2006-3.4.1 |
2. Aerodynamics |
SHEAR CONTROLLED SWIRL JETS BY
HELICAL PERTURBATION WAVE , ICAS 2006-P2.2 |
2. Aerodynamics |
SLAT NOISE PREDICTIONS BASED
ON APE AND STOCHASTIC SOUND SOURCES FROM RANS , ICAS 2006-2.8.2 |
2. Aerodynamics |
SMOOTHED PARTICLE HYDRODYNAMICS
SIMULATION OF FUEL TANK SLOSHING , ICAS 2006-2.7.4 |
2. Aerodynamics |
SONIC BOOM PREDICTION, FOCUSING
AND MITIGATION , ICAS 2006-2.8.3 |
2. Aerodynamics |
STABILIZING A LAMINAR BOUNDARY-LAYER
USING PLASMA-ACTUATORS , ICAS 2006-2.11.2 |
2. Aerodynamics |
SUMMARY OF THE DYNAMIC TEST CAPABILITIES
AT CARIA LOW SPEED WIND TUNNEL , ICAS 2006-3.2.1 |
2. Aerodynamics |
SUPERSONIC LAMINAR FLOW CONTROL
STUDIES IN THE SUPERTRAC PROJECT , ICAS 2006-2.9.1 |
2. Aerodynamics |
SUPERSONIC/TRANSONIC FLOW CONTROL
BY ELECTRO-DISCHARGE PLASMA TECHNIQUE , ICAS 2006-2.11.1 |
2. Aerodynamics |
SURFACE PRESSURE VARIATION ON
AN AIRFOIL IN PLUNGING AND PITCHING MOTIONS , ICAS 2006-3.10.1 |
2. Aerodynamics |
THE AC20.30 BLENDED WING BODY
CONFIGURATION: DEVELOPMENT & CURRENT STATUS 2006 , ICAS 2006-3.7.1 |
2. Aerodynamics |
THE ANALYSIS OF CYCLOGYRO USING
UNSTEADY VORTEX LATTICE METHOD , ICAS 2006-3.6.1 |
2. Aerodynamics |
THE COMPARATIVE EVALUATION OF
POWER REQUIREMENTS FOR FIXED, ROTARY AND FLAPPING WINGS MICRO AIR
VEHICLES , ICAS 2006-P2.13 |
2. Aerodynamics |
THE DESIGN OF ADAPTIVE WINGS USING SPINAL STRUCTURES, ICAS 2006-2.7.5 |
2. Aerodynamics |
THE EFFECT OF GEOMETRY ON THE
PERFORMANCE OF SYNTHETIC JET ACTUATORS , ICAS 2006-P2.11 |
2. Aerodynamics |
THE HIRENASD PROJECT: HIGH REYNOLDS
NUMBER AEROSTRUCTURAL DYNAMICS EXPERIMENTS IN THE EUROPEAN TRANSONIC
WINDTUNNEL (ETW) , ICAS 2006-5.11.2 |
2. Aerodynamics |
TRANSITION MEASUREMENT SYSTEM
OF EXPERIMENTAL SUPERSONIC TRANSPORT “NEXST-1” , ICAS 2006-3.3.2 |
2. Aerodynamics |
TRENDS FOR LOW NOISE HIGH-LIFT DESIGN DERIVED FROM WIND-TUNNEL
TESTS, ICAS 2006-2.8.1 |
2. Aerodynamics |
TURBULENT BOUNDARY LAYER FLOW
OVER CIRCULAR CAVITIES , ICAS 2006-2.7.2 |
2. Aerodynamics |
TURBULENT FLOW CONTROL BY ELECTROMAGNETIC
FORCES , ICAS 2006-2.9.2 |
2. Aerodynamics |
UNSTEADY AERODYNAMIC ANALYSIS OF WINGS FLYING OVER NONPLANAR
GROUND SURFACES, ICAS 2006-P2.20 |
2. Aerodynamics |
USING CRYOTSP AS A TOOL FOR TRANSITION DETECTION, ICAS 2006-3.3.4 |
2. Aerodynamics |
VALIDATION STUDY OF CFD ANALYSIS
FOR HIGH-LIFT SYSTEMS , ICAS 2006-2.3.1 |
2. Aerodynamics |
WING ROCK CONTROL VIA EXTERNAL EXCITATION, ICAS 2006-P2.21 |
2. Aerodynamics |
3-D FEM
ANALYSIS OF PLASTIC BEHAVIOR INSIDE MMC COMPOSITES CONSIDERING DAMAGE
THEORY , ICAS2006-4.9S |
3. Materials and Structures |
A BREAKTHROUGH IN ASSEMBLY OF
AIRCRAFT COMPOSITE STRUCTURES , ICAS 2006-4.4.5 |
3. Materials and Structures |
A GENERALIZED LOCAL STRAIN APPROACH
TO CONSIDERING THICKNESS EFFECT ON FATIGUE PERFORMANCE ,
ICAS2006-4.3S |
3. Materials and Structures |
A GLOBAL-LOCAL OPTIMIZATION METHOD
FOR PROBLEMS IN STRUCTURAL DYNAMICS , ICAS 2006-4.10.4 |
3. Materials and Structures |
A HOLISTIC APPROACH TO FLUTTER
CLEARANCE USING CLASSICAL METHODS , ICAS 2006-10.3.4 |
3. Materials and Structures |
A HYBRID WAVE BASED VIBRO-ACOUSTIC
MODELLING TECHNIQUE FOR THE PREDICTION OF INTERIOR NOISE IN AN AIRCRAFT
FUSELAGE , ICAS 2006-10.1.3 |
3. Materials and Structures |
A MULTIBODY APPROACH FOR MODELLING
OF THE MANOEUVRING AEROELASTIC AIRCRAFT DURING PRE-DESIGN ,
ICAS 2006-10.2.2 |
3. Materials and Structures |
A NEW CONCEPT FOR TESTING FATIGUE
AND DAMAGE TOLERANCE AT AEROSPACE STRUCTURE , ICAS 2006-4.2.2 |
3. Materials and Structures |
A NEW TYPE OF LIMIT CYCLE OSCILLATION
OCCURRED IN FLUTTER WING MODEL AT TRANSONIC WIND TUNNEL TESTS , ICAS 2006-10.3.2 |
3. Materials and Structures |
A STUDY OF STRUCTURE WEIGHT ESTIMATION
FOR HIGH ALTITUDE LONG ENDURANCE (HALE) UNMANNED AERIAL VEHICLE (UAV)
, ICAS2006-10.1S |
3. Materials and Structures |
ACTIVE AEROELASTIC CONTROL OF
VARIABLE CAMBER AIRFOIL IN THE PRESENCE OF STRUCTURAL NON-LINEARITIES
, ICAS 2006-10.6.1 |
3. Materials and Structures |
ACTUATION CONCEPTS FOR MORPHING
HELICOPTER ROTOR BLADES , ICAS 2006-10.6.4 |
3. Materials and Structures |
ADVANCED CONCEPTS FOR NOVEL LANDING GEAR STRUCTURES
USING HIGHLY ANISOTROPIC COMPOSITES, ICAS2006-4.10S |
3. Materials and Structures |
AEROELASTIC ANALYSIS OF TYPICAL
SECTIONS WITH STRUCTURAL AND AERODYNAMIC NONLINEARITIES , ICAS2006-10.2S |
3. Materials and Structures |
AEROELASTIC CONTROL OF A FLEXIBLE WING WITH EMBEDDED
PIEZOELECTRIC ACTUATORS, ICAS2006-10.6S |
3. Materials and Structures |
AGING PREDICTION OF RUBBER ELEMENT
BY NEURAL NETWORK , ICAS 2006-P3.3 |
3. Materials and Structures |
AIRCRAFT DITCHING NUMERICAL SIMULATION
, ICAS 2006-9.6.2 |
3. Materials and Structures |
AIRCRAFT INTERIOR NOISE REDUCTION
THROUGH A PIEZO TUNABLE VIBRATION ABSORBER SYSTEM , ICAS2006-10.1S |
3. Materials and Structures |
AN ANALYTICAL METHOD IN COMPUTATIONAL
AEROELASTICITY BASED ON WAGNER FUNCTION , ICAS2006-10.3S |
3. Materials and Structures |
AN EXPERIMENTAL STUDY OF THE
STRUCTURAL DAMPING OF THE FULL-SCALE HELICOPTER MAIN ROTOR BLADE FROM
COMPOSITE LAMINATED MATERIALS , ICAS 2006-10.7.3 |
3. Materials and Structures |
ANALYSIS OF THE STATIC AND DYNAMIC
AERO-STRUCTURAL RESPONSE OF AN ELASTIC SWEPT WING MODEL BY DIRECT
AEROELASTIC SIMULATION , ICAS 2006-10.3.3 |
3. Materials and Structures |
APPLICATION OF ELECTRIC POTENTIAL
METHOD ON MONITORING FATIGUE CRACKING OF AIRCRAFT STRUCTURAL ELEMENTS
, ICAS 2006-4.7.4 |
3. Materials and Structures |
ASSESSING THE STRUCTURAL INTEGRITY
OF POAF AIRCRAFT , ICAS 2006-P3.9 |
3. Materials and Structures |
BUCKLING AND POST-BUCKLING OF
SUB-STIFFENED OR LOCALLY TAILORED ALUMINIUM PANELS ,
ICAS 2006-10.4.3 |
3. Materials and Structures |
BUCKLING OF WING SPARS UNDER
COMBINED LOADING , ICAS2006-10.4S |
3. Materials and Structures |
CALCULATION OF F/A-18 FATIGUE
LOADS AND WING DEFORMATION USING COMPUTATIONAL FLUID DYNAMICS ,
ICAS 2006-10.5.2 |
3. Materials and Structures |
CHALLENGES OF THE METALLIC FUSELAGE
, ICAS 2006-4.5.1 |
3. Materials and Structures |
COMPARATIVE EFFICIENCY OF FINITE
ELEMENT MODELS OF CFRP BONDED JOINTS , ICAS 2006-4.11.3 |
3. Materials and Structures |
COMPREHENSIVE DESIGN AND EVALUATION
OF AIRCRAFT STRUCTURAL SYSTEM EFFECTIVENESS , ICAS 2006-4.5.3 |
3. Materials and Structures |
COMPUTATIONAL AND EXPERIMENTAL ASSESSMENT OF CONDITIONS
FOR CUTTING OF ALLOYED STEEL IN HIGH SPEED MILLING, ICAS2006-4.6S |
3. Materials and Structures |
COUPLING TECHNIQUES FOR COMPUTATIONAL
NONLINEAR TRANSIENT AEROELASTICITY , ICAS 2006-10.2.3 |
3. Materials and Structures |
CRASHWORTHINESS OF AIRCRAFT SEAT
, ICAS 2006-P3.13 |
3. Materials and Structures |
CROSS-PLY BENDING AND STABILITY
OF COMPRESSED BAR WITH CRACK , ICAS 2006-P3.7 |
3. Materials and Structures |
CYCLIC BUCKLING TESTS OF CFRP
CURVED PANELS , ICAS 2006-10.4.5 |
3. Materials and Structures |
DELAMINATION GROWTH RATE AT LOW
AND ELEVATED TEMPERATURES IN GLARE , ICAS2006-4.1S |
3. Materials and Structures |
DESIGN IMPROVEMENT BY SHAPE CHANGE
USING A LINEAR FINITE ELEMENT METHOD , ICAS 2006-4.10.2 |
3. Materials and Structures |
DESIGN OF HIGHLY REFLECTIVE TBC
SYSTEM FOR GAS TURBINE APPLICATION , ICAS 2006-4.6.3 |
3. Materials and Structures |
DESIGN, OPTIMIS ATION AND TECHNOLOGY
OF CARBON COMPOSITE AXIAL FLOW FAN ROTOR BLADE OF LIGHT AIRCRAFT PROPULSION
SYSTEM , ICAS2006-4.8S |
3. Materials and Structures |
DEVELOPMENT AND APPLICATION OF
A NEW DESIGN TOOL FOR AEROSPACE STRUCTURES , ICAS 2006-4.10.5 |
3. Materials and Structures |
DEVELOPMENT OF ADVANCED LAMINATES
FOR AIRCRAFT STRUCTURES , ICAS 2006-4.1.3 |
3. Materials and Structures |
DEVELOPMENT OF FASTENER MODELS
FOR IMPACT SIMULATION OF COMPOSITE STRUCTURES , ICAS2006-10.7S |
3. Materials and Structures |
DYNAMIC LOADS OF CONTROL SYSTEM
ELEMENTS , ICAS2006-10.6S |
3. Materials and Structures |
DYNAMIC STRENGTH TESTING OF 3D-REINFORCED
T-JOINTS , ICAS 2006-4.4.4 |
3. Materials and Structures |
EFFECTS OF GEOMETRY ASPECTS ON
THE SIMULATION OF SUPERPLASTICITY IN MMC COMPOSITES , ICAS 2006-P3.12 |
3. Materials and Structures |
EFFICIENT PREDICTION OF COMPOSITE
DAMAGE TOLERANCE , ICAS 2006-4.3.2 |
3. Materials and Structures |
EXPERIMENTAL AND NUMERICAL INVESTIGATION
ON THE FAILURE MODES OF THICK COMPOSITE LAMINATES ,
ICAS 2006-4.8.2 |
3. Materials and Structures |
EXPERIMENTAL CONFIRMATION OF
LIMIT CYCLE OSCILLATION FOR ACTIVE CONTROL OF TRANSONIC FLUTTER IN
WIND TUNNEL , ICAS 2006-10.2.1 |
3. Materials and Structures |
FATIGUE INITIATION AND CRACK
GROWTH BEHAVIOUR IN GLARE FROM THE AIRBUS MEGALINER BARREL TEST ,
ICAS 2006-4.1.2 |
3. Materials and Structures |
FATIGUE PROPERTIES OF Z-PINNED
AIRCRAFT COMPOSITE MATERIALS , ICAS 2006-4.2.3 |
3. Materials and Structures |
FINITE ELEMENT ANALYSIS OF FRICTION STIR WELDING TEMPERATURE
FIELD, ICAS 2006-P3.2 |
3. Materials and Structures |
FINITE ELEMENT ANALYSIS FOR THROUGH
THICKNESS REINFORCEMENT REPAIR OF DELAMINATED CARBON-EPOXY PANELS
,
ICAS 2006-4.5.2 |
3. Materials and Structures |
FLUTTER ANALYSIS OF KF-16 AIRCRAFT
UTILIZING TEST MODAL DATA , ICAS 2006-P3.8 |
3. Materials and Structures |
FUTURE DESIGN SCENARIO FOR COMPOSITE
AIRFRAME PANELS , ICAS 2006-10.4.1 |
3. Materials and Structures |
GLOBAL-LOCAL ANALYSIS OF BONDED
SKIN-TO-STIFFENER JOINTS IN POST-BUCKLED PANELS , ICAS 2006-4.11.2 |
3. Materials and Structures |
HEALTH MONITORING OF AIRCRAFT
FUSELAGE STRUCTURES USING ULTRASONIC WAVES , ICAS 2006-4.7.3 |
3. Materials and Structures |
HYBRID FABRICATION ROUTE- COST EFFICIENT CFRP PRIMARY
AIRFRAME STRUCTURES , ICAS 2006-4.8.1 |
3. Materials and Structures |
IMPACT DAMAGE MODELLING OF COMPOSITE
AEROSPACE STRUCTURES SUBJECT TO BIRD-STRIKE , ICAS 2006-10.7.1 |
3. Materials and Structures |
IMPACT OF BONDED REPAIRS TO CFRP
LAMINATES UNDER LOAD , ICAS 2006-4.2.4 |
3. Materials and Structures |
IMPROVEMENT OF THE SOUND TRANSMISSION
LOSS OF PANELS BY MEANS OF ACOUSTICALLY TUNED RESONATORS ,
ICAS 2006-10.1.2 |
3. Materials and Structures |
INERTIA FORCES ROLE IN STATIC
AEROELASTICITY , ICAS 2006-10.3.1 |
3. Materials and Structures |
INFLUENCE OF DIFFERENT STIFFENING
TYPES OF THE AIRCRAFT BODY STRUCTURE ON THE NOISE EXPOSURE IN THE
CABIN , ICAS 2006-10.1.1 |
3. Materials and Structures |
INFLUENCE OF HIGH PERFORMANCE
CUTTING OPERATIONS ON THE RESIDUAL STRESSES OF ALUMINUM STRUCTURAL
WORKPIECES , ICAS 2006-4.6.4 |
3. Materials and Structures |
INTEGRATED DESIGN OF SMART COMPOSITES
APPLIED TO SMART WINGLETS , ICAS 2006-10.6.3 |
3. Materials and Structures |
INTEGRATED VEHICLE HEALTH MANAGEMENT SYSTEMS, ICAS 2006-4.7.1 INVITED: |
3. Materials and Structures |
INVERSE METHODS FOR DAMAGE IDENTIFICATION IN AERONAUTICAL
STRUCTURES, ICAS 2006-4.7.2 |
3. Materials and Structures |
INVESTIGATING AND MODELING OF
THE MULTI-AXIAL FATIGUE AND COMPLEX DEFORMATION OF A NI-BASED SUPERALLOY
FOR IMPROVING DISC LIFING , ICAS 2006-4.6.2 |
3. Materials and Structures |
INVESTIGATION OF WAVE PROPAGATION
IN COMPOSITES AS REQUIREMENT FOR IMPACT DETECTION , ICAS2006-4.2S |
3. Materials and Structures |
KOITER’S POSTBUCKLING ANALYSIS
OF GENERAL SHELL STRUCTURES USING THE FINITE ELEMENT METHOD ,
ICAS 2006-4.11.1 |
3. Materials and Structures |
LIQUID COMPOSITE MOULDING FOR
AERONAUTICAL STRUCTURES , ICAS 2006-4.4.2 |
3. Materials and Structures |
LQG FLUTTER CONTROL OF WIND TUNNEL
MODEL USING PIEZO-CERAMIC ACTUATOR , ICAS 2006-10.6.2 |
3. Materials and Structures |
MAGNESIUM CASTINGS FOR AIRCRAFTS
, ICAS 2006-4.9.3 |
3. Materials and Structures |
MATRIX FORMULATION FOR CALCULATIONS
OF WING LOADING DISTRIBUTION , ICAS 2006-10.5.3 |
3. Materials and Structures |
MEASUREMENT OF RESIDUAL STRESSES
IN ALUMINIUM ALLOY AEROSPACE COMPONENTS , ICAS 2006-P3.5 |
3. Materials and Structures |
MEASURES AND TEST TECHNIQUES
OF FUNGUS RESISTANCE TO AIRCRAFT MATERIALS AND EQUIPMENT ,
ICAS 2006-P3.1 |
3. Materials and Structures |
MICRO-MECHANICAL MODEL OF A SINGLE
CRYSTAL NICKEL-BASE SUPERALLOY , ICAS 2006-4.9.1 |
3. Materials and Structures |
MICROWAVE TECHNOLOGIES FOR COMPOSITE
PROCESSING , ICAS 2006-4.4.3 |
3. Materials and Structures |
MULTI-DIMENSION LAPLACE WAVELET
AND THE APPLICATIONS IN FLIGHT FLUTTER TEST , ICAS 2006-P3.6 |
3. Materials and Structures |
MULTIDISCIPLINARY OPTIMISATION
OF CFRP FUSELAGES: STRUCTURAL MECHANICS, VIBRO-ACOUSTICS AND MANUFACTURING
ASPECTS , ICAS2006-4.10S |
3. Materials and Structures |
NANOTECHNOLOGY FOR NOVEL HIGH-PERFORMANCE
COMPOSITES: MANUFACTURING, CHARACTERIZATION AND APPLICATION ,
ICAS 2006-P3.15 |
3. Materials and Structures |
NON LINEAR AEROELASTIC BEHAVIOR
OF HIGHLY FLEXIBLE HALE WINGS , ICAS 2006-10.2.4 |
3. Materials and Structures |
NUMERICAL SIMULATION OF C-141
LOWER WING PANELS WITH AND WITHOUT SIMULATED EXFOLIATION CORROSION
UNDER COMPRESSION , ICAS 2006-4.9.4 |
3. Materials and Structures |
NUMERICAL SIMULATION OF THE STRUCTURAL
BEHAVIOUR OF ORTOTHROPICALLY STIFFENED AIRCRAFT PANELS UNDER SHORT
TIME DURATION LOADING , ICAS 2006-10.7.5 |
3. Materials and Structures |
OPTIMISATION OF ENERGY ABSORBING
SUBSYSTEM FOR HELICOPTER VERTICAL CRASHES , ICAS 2006-10.7.4 |
3. Materials and Structures |
OPTIMIZATION OF COMPOSITE AIRCRAFT
PANELS USING EFFICIENCY ENHANCING EVOLUTIONARY ALGORITHMS ,
ICAS 2006-4.10.3 |
3. Materials and Structures |
POSTBUCKLING BEHAVIOUR OF A STIFFENED
PANEL SUBJECT TO COMBINED LOADING , ICAS 2006-10.4.4 |
3. Materials and Structures |
PROBABILISTIC DESIGN OF ADVANCED
COMPOSITE MATERIALS FOR AEROSPACE STRUCTURES , ICAS 2006-4.3.4 |
3. Materials and Structures |
PROCESS INTERACTIONS AND FATIGUE
LIFE , ICAS 2006-4.2.1 |
3. Materials and Structures |
PROGRESS ON AIRCRAFT INTEGRATED
SAFETY HEALTH ASSESSMENT (AISHA) , ICAS 2006-P3.11 |
3. Materials and Structures |
RELIABILITY ANALYSIS IN BOLTED
COMPOSITE JOINTS WITH SHIMMING MATERIAL , ICAS 2006-4.3.3 |
3. Materials and Structures |
RTM COMPOSITE LUGS FOR HIGH LOAD
TRANSFER APPLICATIONS , ICAS 2006-4.4.1 |
3. Materials and Structures |
SIMULATION OF STRUCTURAL BEHAVIOUR
OF FIBRE METAL LAMINATE JOINTS , ICAS2006-4.11S |
3. Materials and Structures |
SMART VORTEX GENERATOR USING
SHAPE MEMORY ALLOY , ICAS 2006-4.7.5 |
3. Materials and Structures |
STRESS STAT IN THE RIVET JOINTS:
THE APPLIED THEORY OF THE FATIGUE FRACTURE , ICAS 2006-4.3.1 |
3. Materials and Structures |
STRUCTURAL BEHAVIOR OF DAMAGED
ANISOTROPIC STIFFENED PANELS UNDER COMPRESSIVE LOADS , ICAS2006-4.8S |
3. Materials and Structures |
STUDY OF FUNDAMENTAL LAMB MODES
BEHAVIOUR WITH A SHARP CHANGE OF SECTION IN A PLATE , ICAS 2006-P3.4 |
3. Materials and Structures |
SYNTHESIS AND CHARACTERISATION
OF NANO-AL2O3 REINFORCED AA6061 , ICAS 2006-4.9.2 |
3. Materials and Structures |
TAILORED FIBRE PLACEMENT OPTIMIZATION
TOOL , ICAS 2006-4.8.3 |
3. Materials and Structures |
TESTING AND MODELING OF FAILURE
BEHAVIOR ON FIBER METAL LAMINATES , ICAS 2006-4.1.1 |
3. Materials and Structures |
THE DYNAMIC RESPONSE OF LAMINATE
COMPOSITE PLATE UNDER LOW-VELOCITY IMPACT , ICAS 2006-P3.14 |
3. Materials and Structures |
THE EU-FUNDED “ ULTMAT ” PROJECT:
ULTRA HIGH TEMPERATURE MATERIALS FOR TURBINES , ICAS 2006-P3.17 |
3. Materials and Structures |
THE MANUFACTURING TECHNOLOGY
OF AN ULTRA-PRECISION AEROSTATIC SPINDLE SYSTEM , ICAS 2006-P3.10 |
3. Materials and Structures |
THE ROLE OF OPTIMIZATION IN COMPONENT
STRUCTURAL DESIGN: APPLICATION TO THE F-35 JOINT STRIKE FIGHTER ,
ICAS 2006-4.10.1 |
3. Materials and Structures |
THE SAILPLANE COCKPIT STRUCTURE
DURING EMERGENCY LANDING CONDITION , ICAS 2006-10.5.1 |
3. Materials and Structures |
THERMAL ANALYSIS OF HYBRID COMPOSITE
STRUCTURES , ICAS 2006-4.6.1 |
3. Materials and Structures |
THROUGH THICKNESS MICROSTRUCTURAL GRADIENTS IN 7475
AND 2022 AGEFORMED BEND COUPONS FOR FUSELAGE AND LOWER WING SKIN APPLICATIONS, ICAS 2006-P3.16 |
3. Materials and Structures |
TOWARDS A METHODOLOGY FOR THE
DESIGN OF BIRD-PROOF INTAKES MADE WITH COMPOSITE MATERIAL , ICAS 2006-10.7.2 |
3. Materials and Structures |
VALIDATION PROCEDURE FOR NONLINEAR
ANALYSIS OF STRINGER STIFFENED CFRP PANELS , ICAS 2006-10.4.2 |
3. Materials and Structures |
3D FULL
PREDICTIVE THERMAL CHAIN FOR GAS TURBINE COMBUSTOR METAL TEMPERATURE
, ICAS 2006-5.5.1 |
4. Propulsion |
A TEST RIG FOR INVESTIGATIONS
OF GAS TURBINE COMBUSTOR COOLING CONCEPTS UNDER REALISTIC OPERATING
CONDITIONS , ICAS 2006-5.3.3 |
4. Propulsion |
AEROELASTIC SIMULATION OF S-DUCT
DYNAMICS USING STRUCTURE-COUPLED CFD , ICAS 2006-5.1.3 |
4. Propulsion |
AERO-ENGINE TECHNOLOGY TO COPE
WITH ACARE GOALS , ICAS 2006-5.4.5 |
4. Propulsion |
ALTERNATE FUELS AND THEIR POTENTIAL
IMPACT TO AVIATION , ICAS 2006-5.8.2 (ISABE): |
4. Propulsion |
ANALYSIS OF INCREASED COMPRESSION
FACTOR ON EJECTOR-ROCKET PERFORMANCE , ICAS 2006-5.2.2 |
4. Propulsion |
APPLICATIONS OF GAME THEORY IN
A SYSTEMS DESIGN APPROACH TO STRATEGIC ENGINE SELECTION , ICAS 2006-5.4.1 |
4. Propulsion |
CHALLENGES IN THE HARDWARE IN THE LOOP SIMULATION FOR
AN AERO GAS TURBINE ENGINE CONTROL SYSTEM, ICAS 2006-5.4.2 |
4. Propulsion |
CLEAN- Validation of a GTF High Speed Turbine and Integration
of Heat Exchanger Technology in an Environmental Friendly Engine Concept,
ICAS 2006-8.10.3 |
4. Propulsion |
COMPRESSOR STABILITY MANAGEMENT
IN AIRCRAFT ENGINES , ICAS2006-5.6S |
4. Propulsion |
COMPUTATION OF FLOW AND HEAT TRANSFER IN A PRESWIRL
ROTOR-STATOR SYSTEM, ICAS2006-5.1S |
4. Propulsion |
CONTROL OF SUPERSONIC INLET WITH
VARIABLE RAMP , ICAS 2006-5.2.4 |
4. Propulsion |
DERIVATION OF AERODYNAMIC THRUST
CORRECTION FOR AN INDOOR GAS TURBINE ENGINE TEST FACILITY USING THE
"FIRST PRINCIPLES" ANEMOMETER METHOD , ICAS 2006-5.6.4 |
4. Propulsion |
DEVELOPMENT OF A COMBUSTION CHAMBER
DESIGN METHODOLOGY AND AUTOMATION OF THE DESIGN PROCESS ,
ICAS2006-5.5S |
4. Propulsion |
Development of Air Breathing Engine Theory in Russia: Past, Present and Future , ICAS 2006-8.10.2 |
4. Propulsion |
DEVELOPMENTS IN LOW EMISSIONS COMBUSTION TECHNOLOGY
FOR AERO ENGINE APPLICATIONS, ICAS 2006-5.5.3 |
4. Propulsion |
Economy, Profitability and Environmental Compatibility:
Challenges in Future Civil Air Transportation; Results of the XVII
ISABE Panel Discussion, ICAS 2006-8.9.4 |
4. Propulsion |
EFFECTS OF GAS RADIATION IN SCALED COOLING EFFECTIVENESS
TESTS OF TURBINE VANES, ICAS 2006-P4.3 |
4. Propulsion |
Engine Technology Prepared in Europe- Innovation by Successful
Partnerships, ICAS 2006-8.9.1 |
4. Propulsion |
INTERMEDIATE TURBINE DUCT DESIGN
AND OPTIMIZATION , ICAS 2006-5.1.1 |
4. Propulsion |
INVESTIGATION OF A COMBUSTOR
USING A PRESUMED JPDF REACTION MODEL APPLYING RADIATIVE HEAT LOSS
BY THE MONTE CARLO METHOD , ICAS 2006-5.3.2 |
4. Propulsion |
LOW EMISSIONS COMBUSTOR TECHNOLOGY
DEVELOPMENTS IN THE EUROPEAN PROGRAMMES LOPOCOTEP AND TLC ,
ICAS 2006-5.5.2 |
4. Propulsion |
MULTIDISCIPLINARY COMPRESSOR
BLADING DESIGN PROCESS USING AUTOMATION AND MULTI-OBJECTIVE OPTIMIZATION
, ICAS2006-5.6S |
4. Propulsion |
MULTIPLE NOZZLE COCEPT IN A SINGLE
ENGINE , ICAS 2006-P4.1 |
4. Propulsion |
MULTIPLE NOZZLE COCEPT IN A SINGLE
ENGINE , ICAS2006-5.5S |
4. Propulsion |
NUMERICAL COMPUTATIONS FOR DESIGNING
A SCRAMJET INTAKE , ICAS 2006-5.2.3 |
4. Propulsion |
OPTIMIZATION LOOP BASED ON A
CFD RANS CODE , ICAS 2006-5.3.1 |
4. Propulsion |
OPTIMUM PITCH ANGLE IN ENGINE
INSTALLATION OF A CIVIL JET AIRCRAFT, ICAS 2006-5.4.3 |
4. Propulsion |
PARAMETRIC INTERTURBINE DUCT
DESIGN AND OPTIMISATION , ICAS 2006-5.1.2 |
4. Propulsion |
POA ENGINE SYSTEM VALIDATION RIG – AIMS AND CHALLENGES,
ICAS 2006-5.6.2 |
4. Propulsion |
Propulsion Systems and Technologies for Future Manned
and Unmanned Aerial Vehicles, ICAS 2006-8.10.4 |
4. Propulsion |
RECENT ADVANCES IN THE SIMULATION
OF GAS TURBINE SECONDARY AIR SYSTEMS , ICAS 2006-5.4.4 |
4. Propulsion |
RESEARCH AND TECHNOLOGY AT SNECMA
TO ENSURE SUSTAINED DEVELOPMENT OF AIR TRANSPORTATION , ICAS 2006-8.9.3 |
4. Propulsion |
STAGNATION-POINT REVERSE FLOW
COMBUSTOR PERFORMANCE WITH LIQUID FUEL INJECTION , ICAS 2006-5.3.4 |
4. Propulsion |
THE AITEB PROGRAMME: EUROPEAN RESEARCH FOR IMPROVED
HIGH PRESSURE TURBINES, ICAS2006-5.4S |
4. Propulsion |
The Environmental Challenge- Bringing Technology to
Market,
ICAS 2006-8.9.2 |
4. Propulsion |
THE FEASIBILITY OF THE SCRAMJET:
AN ANALYSIS BASED ON FIRST PRINCIPLES , ICAS 2006-5.2.1 |
4. Propulsion |
THE INFLUENCE OF FLAME HOLDER GEOMETRY ON THE THRUST
INSTABILITY IN A LABORATORIAL SCALE RAMJET ENGINE, ICAS 2006-P4.2 |
4. Propulsion |
TWO SPOOL MORE ELECTRICAL ENGINE, ICAS 2006-5.6.3 |
4. Propulsion |
Validation Methodology for the
Development of Low Emission Fuel Injectors for Aero Engines ,
ICAS 2006-8.10.5 |
4. Propulsion |
VALIDATION OF PROPULSION TECHNOLOGIES
AND NEW ENGINE CONCEPTS IN A JOINT TECHNOLOGY DEMONSTRATOR PROGRAM
, ICAS 2006-8.10.1 |
4. Propulsion |
VITAL, AN EUROPEAN R&D PROGRAM
FOR GREENER AERO-ENGINES , ICAS 2006-5.6.1 |
4. Propulsion |
A NEW APPROACH
TO NONLINEAR MODELING OF HIGHLY MANEUVERABLE AIRCRAFT USING NEURAL
NETWORKS ,
ICAS 2006-6.5.3 |
5. Flight Dynamics and Control |
A NEW ARCHITECTURE TO HARMONIZE
AUTOMATION WITH PILOT MANEUVER , ICAS 2006-6.9.2 |
5. Flight Dynamics and Control |
ACTUATOR INFLUENCE ON FLYING
QUALITIES OF A NATURALLY UNSTABLE AIRCRAFT , ICAS 2006-6.9.4 |
5. Flight Dynamics and Control |
ADAPTIVE NODE DISTRIBUTION FOR
ON-LINE TRAJECTORY PLANNING , ICAS 2006-6.3.2 |
5. Flight Dynamics and Control |
AIRCRAFT HEADING CONTROL IN CASE OF INCOMPLETE MEASUREMENT
INFORMATION FOR FLY-BY-WIRE CONTROL SYSTEM, ICAS 2006-P5.6 |
5. Flight Dynamics and Control |
AUTONOMOUS TAKE OFF AND LANDING
OF THE SHARC TECHNOLOGY DEMONSTRATOR , ICAS 2006-6.7.2 |
5. Flight Dynamics and Control |
BELL M427 FLIGHT TEST DATA GATHERING
AND LEVEL-D SIMULATOR MODEL DEVELOPMENT , ICAS 2006-6.10.1 |
5. Flight Dynamics and Control |
CONCEPTION OF AN UAV GENERIC
MISSION SYSTEM , ICAS 2006-6.8.1 |
5. Flight Dynamics and Control |
CONTROL SYSTEM DESIGN FOR AN
AUTONOMOUS HELICOPTER USING PARTICLE SWARM OPTIMIZATION , ICAS 2006-6.7.4 |
5. Flight Dynamics and Control |
CURVED AND STEEP APPROACH FLIGHT
TESTS OF A LOW-COST 3D-DISPLAY FOR GENERAL AVIATION AIRCRAFT ,
ICAS 2006-6.2.2 INVITED: |
5. Flight Dynamics and Control |
DESIGN OF A TRACKING CONTROL
SYSTEM FOR AN OPTIMAL POST-STALL MANOEUVRE USING DYNAMIC INVERSION
APPROACH , ICAS 2006-6.7.3 |
5. Flight Dynamics and Control |
DEVELOPMENT OF A LOW COST FLIGHT DYNAMIC TEST CAPABILITY
FOR UAV, ICAS2006-6.8S |
5. Flight Dynamics and Control |
DEVELOPMENT OF CONTROL LAWS FOR
THE SIMULATION OF A NEW TRANSPORT AIRCRAFT , ICAS 2006-6.2.3 |
5. Flight Dynamics and Control |
DEVELOPMENT OF LIGHT AIRCRAFT
FLIGHT TEST EQUIPMENT , ICAS2006-6.2S |
5. Flight Dynamics and Control |
DEVELOPMENT OF THE CONTROL
BASED ON THE BIOLOGICAL PRINCIPLES,
ICAS 2006-6.4.3 |
5. Flight Dynamics and Control |
FAULT IMMUNE FLIGHT CONTROL SYSTEM
FOR CIVIL TRANSPORTS , ICAS 2006-6.4.2 |
5. Flight Dynamics and Control |
FLIGHT CONTROL WITH MINIATURE
TRAILING EDGE EFFECTORS , ICAS 2006-6.4.1 |
5. Flight Dynamics and Control |
FLIGHT DYNAMIC SIMULATION OF
A FLAPLESS FLIGHT CONTROL UAV , ICAS 2006-6.8.2 |
5. Flight Dynamics and Control |
FLIGHT PLAN AND FLIGHT TEST RESULTS
OF EXPERIMENTAL SST VEHICLE NEXST-1 , ICAS 2006-6.2.1 INVITED: |
5. Flight Dynamics and Control |
FLIGHT SIMULATION FOR THE PC-21
PROJECT , ICAS 2006-6.10.5 |
5. Flight Dynamics and Control |
FORMATION FLIGHT DESIGN ASPECTS, ICAS 2006-6.6.1 INVITED: |
5. Flight Dynamics and Control |
FULL ENVELOPE MISSILE AUTOPILOT DESIGN, ICAS2006-6.1S |
5. Flight Dynamics and Control |
GENERALIZED MISSILE GUIDANCE
LAWS AGAINST MANEUVERING TARGETS , ICAS 2006-6.1.3 |
5. Flight Dynamics and Control |
HELICOPTER LOW LEVEL FLIGHT USING
TRAJECTORY PLANNING AND OBSTACLE AVOIDANCE , ICAS 2006-6.3.1 |
5. Flight Dynamics and Control |
INTELLIGENT BASED TRAJECTORY
PLANNING IN TERRAIN FOLLOWING FLIGHT , ICAS 2006-6.3.3 |
5. Flight Dynamics and Control |
METHOD AND INTEGRATED TOOLS FOR
EFFICIENT DESIGN OF AIRCRAFT CONTROL SYSTEMS , ICAS 2006-6.7.5 |
5. Flight Dynamics and Control |
METHOD FOR CALCULATING OBSERVABILITY
OF AIRCRAFT FLIGHT ROUTE , ICAS 2006-6.3.4 |
5. Flight Dynamics and Control |
MINC: A MINIATURE INTEGRATED
GUIDANCE, NAVIGATION & CONTROL SYSTEM ENABLES IN-FLIGHT GPS/INS
DATA FUSION ABOARD A MICRO AERIAL VEHICLE , ICAS 2006-6.11.1 |
5. Flight Dynamics and Control |
MODEL REDUCTION FOR GPS/SINS
INTEGRATED NAVIGATION SYSTEM USING KRYLOV SUBSPACE METHODS ,
ICAS 2006-6.11.2 |
5. Flight Dynamics and Control |
MULTI-AGENT FORMATION CONTROL
FOR UAV SWARMING , ICAS 2006-6.6.2 |
5. Flight Dynamics and Control |
MULTI-BODY MODEL OF FLYING WINGS
WITH SIGNIFICANT DEFORMATION , ICAS 2006-6.5.2 |
5. Flight Dynamics and Control |
NEURO-FUZZY CONTROL SYNTHESIS
FOR ELECTROHYDRAULIC SERVOS ACTUATING PRIMARY FLIGHT CONTROLS ,
ICAS 2006-6.4.4 |
5. Flight Dynamics and Control |
NEW PRINCIPLE FOR MISSILE GUIDANCE
AND CONTROL , ICAS 2006-6.1.1 INVITED: |
5. Flight Dynamics and Control |
NONLINEAR MODELING AND SIMULATION OF SMALL-SIZE HELICOPTER
DYNAMICS AND MODEL VALIDATION, ICAS 2006-P5.7 |
5. Flight Dynamics and Control |
ON FLIGHT DYNAMICS MODEL IDENTIFICATION
AND OPTIMAL FLIGHT TEST PROTOCOL DESIGN , ICAS 2006-6.10.3 |
5. Flight Dynamics and Control |
ON THE EFFECT OF DAMPING AND
CONTROLS ON AN AIRCRAFT WAKE ENCOUNTER , ICAS 2006-P5.3 |
5. Flight Dynamics and Control |
OPTIMUM FLIGHT TRAJECTORIES AND
SENSITIVITY ANALYSIS FOR TERRAIN COLLISION AVOIDANCE SYSTEMS ,
ICAS2006-6.3S |
5. Flight Dynamics and Control |
PARAMETRIC ESTIMATION FLIGHT
TEST MANEUVER OPTIMIZATION CONSIDERING MEASUREMENT COLORED RESIDUALS
,
ICAS 2006-6.10.4 |
5. Flight Dynamics and Control |
POSSIBILITIES AND METHODS OF IN FLIGHT LOADING MEASUREMENTS, ICAS2006-6.2S |
5. Flight Dynamics and Control |
PRECISION POINTING OF A PAYLOAD SUSPENDED FROM A HIGH
ALTITUDE BALLOON, ICAS 2006-6.8.3 |
5. Flight Dynamics and Control |
PREDICTIVE FUNCTIONAL CONTROL
AND ITS APPLICATION TO MISSILE CONTROL SYSTEM , ICAS 2006-6.1.2 |
5. Flight Dynamics and Control |
PROGRESS IN PILOT–IN–THE LOOP
INVESTIGATIONS FOR FLYING QUALITIES PREDICTION AND EVALUATION , ICAS 2006-6.9.1 |
5. Flight Dynamics and Control |
PROPELLER INSTALLATION EFFECTS
ON MULTI-ENGINE PROPELLER AIRCRAFT DIRECTIONAL STABILITY AND CONTROL
,
ICAS 2006-6.10.2 |
5. Flight Dynamics and Control |
REAL TIME PREDICTION OF SHIP
MOTION FOR THE AID OF HELICOPTER AND AIRCRAFT DEPLOYMENT AND RECOVERY
,
ICAS 2006-P5.4 |
5. Flight Dynamics and Control |
ROBUST CONTROLLERS DESIGN STRATEGIES
FOR UNMANNED AIR VEHICLES , ICAS 2006-P5.5 |
5. Flight Dynamics and Control |
ROBUST FLIGHT CONTROL SYSTEM DESIGN WITH GUARANTEED
H-INFINITY TYPE PERFORMANCE, ICAS2006-6.7S |
5. Flight Dynamics and Control |
SEVERAL NEW APPROACHES FOR FAULT
TOLERANT FLIGHT CONTROL SYSTEM , ICAS 2006-6.7.1 INVITED: |
5. Flight Dynamics and Control |
STABILITY AND FLYING QUALITIES
ASSESSMENTS OF A SMALL WING-IN-SURFACE-EFFECT TRANSPORT VEHICLE ,
ICAS 2006-6.5.1 |
5. Flight Dynamics and Control |
STATISTICAL FAULT DETECTION AND
IDENTIFICATION IN AIRCRAFT SYSTEMS VIA FUNCTIONALLY POOLED NONLINEAR
MODELLING OF FLIGHT DATA DEPENDENCIES , ICAS 2006-6.2.4 |
5. Flight Dynamics and Control |
THE A380 FLIGHT CONTROL SYSTEM : NEW BREAK THROUGH FOR
NEW CHALLENGES, ICAS 2006-6.4.5 |
5. Flight Dynamics and Control |
THE APPLICATION OF GAUSSIAN COMPLEX
WAVELET IN PIO DETECTION , ICAS 2006-6.9.3 |
5. Flight Dynamics and Control |
THE INFLUENCE OF FREE- PLAY
AND FRICTION IN ELEVATOR CONTROL SYSTEM ON LONGITUDAL DYNAMICS OF
THE STRIKE AIRCRAFT , ICAS 2006-P5.2 |
5. Flight Dynamics and Control |
THE STUDY OF INTEGRATED FIRE/FLIGHT/PROPULSION
CONTROL (IFFPC) SYSTEM AND DESIGN OF DIGITAL SIMULATION/DESIGN PLATFORM
, ICAS 2006-P5.1 |
5. Flight Dynamics and Control |
THROUGH OPTIMIZATION OF BRANCHED
TRAJECTORIES WITH RANDOM DISTURBANCES BY THE PONTRYAGIN MAXIMUM PRINCIPLE
, ICAS 2006-6.6.3 |
5. Flight Dynamics and Control |
Title: TBD, ICAS 2006-10.8.1 INVITED: |
5. Flight Dynamics and Control |
Title: TBD, ICAS 2006-10.8.2 INVITED: |
5. Flight Dynamics and Control |
Title: TBD, ICAS 2006-10.8.3 INVITED: |
5. Flight Dynamics and Control |
3 AIRCRAFT
JOINT TEST TECHNIQUES FOR AIR-TO-AIR SEMI-ACTIVE RADAR-GUIDED MISSILE
RADIO FREQUENCY INTERFACE , ICAS 2006-P6.3 |
6. Systems, Subsystems and Equipments |
A COMPARISON OF SOLID OXIDE FUEL
CELL DESIGNS AS ENERGY SOURCE FOR THE ALL-ELECTRIC AIRCRAFT ,
ICAS 2006-7.7.2 |
6. Systems, Subsystems and Equipments |
A NEW HIGH POWER DENSITY GENERATION
SYSTEM , ICAS 2006-7.1.1 |
6. Systems, Subsystems and Equipments |
ADAPTIVE LANDING GEARS, ICAS 2006-7.11.3 |
6. Systems, Subsystems and Equipments |
ADVANCED OIL SYSTEM FOR THE ANTLE/POA
DEMONSTRATION PLATFORMS , ICAS 2006-7.4.5 |
6. Systems, Subsystems and Equipments |
ADVANCED VERIFICATION AND TEST
METHODS FOR DISTRIBUTED CONTROL ARCHITECTURES IN WATER/WASTE SYSTEMS
,
ICAS 2006-7.6.4 |
6. Systems, Subsystems and Equipments |
AIRCRAFT FUEL SYSTEM DIAGNOSTIC
FAULT DETECTION THROUGH EXPERT SYSTEM , ICAS 2006-P6.2 |
6. Systems, Subsystems and Equipments |
AN ELECTRIC COOLING SYSTEM FOR
AN UAV , ICAS 2006-7.7.3 |
6. Systems, Subsystems and Equipments |
AN ELECTRICAL FUEL PUMPING AND
METERING SYSTEM FOR MORE ELECTRICAL AERO-ENGINES , ICAS 2006-7.4.4 |
6. Systems, Subsystems and Equipments |
AN INNOVATIVE CABIN RECIRCULATION FAN DEMONSTRATOR, ICAS 2006-P6.5 |
6. Systems, Subsystems and Equipments |
AN INNOVATIVE TOOL FOR AIRCRAFT EQUIPMENT SYSTEMS INTEGRATION
AND ELECTRICAL NETWORK CHARACTERISATION, ICAS2006-7.2S |
6. Systems, Subsystems and Equipments |
AN INTEGRATED MACHINE AND MATRIX
CONVERTER BASED HIGH POWER RUDDER EMA , ICAS 2006-7.4.3 |
6. Systems, Subsystems and Equipments |
ANALYSIS OF A FEASIBLE PULSED-POWER
SUPPLY SYSTEM FOR AN UNMANNED AERIAL VEHICLE , ICAS 2006-7.1.3 |
6. Systems, Subsystems and Equipments |
ANALYSIS OF AIRCRAFT COMPRESSOR
SYSTEMS , ICAS 2006-7.7.5 |
6. Systems, Subsystems and Equipments |
AVIONIC OPTICAL LINKS FOR HIGH
DATA-RATE COMMUNICATIONS , ICAS 2006-7.9.1 |
6. Systems, Subsystems and Equipments |
CLOSED-LOOP SIMULATION WITH FLIGHT CONTROL ACTUATORS, ICAS 2006-7.10.5 |
6. Systems, Subsystems and Equipments |
COMPARISON OF POWER QUALITY SOLUTIONS
USING ACTIVE AND PASSIVE RECTIFICATION FOR MORE ELECTRIC AIRCRAFT
, ICAS 2006-7.5.2 |
6. Systems, Subsystems and Equipments |
CONSIDERATION OF FUEL CONSUMPTION
CAUSED BY AIRCRAFT SYSTEMS IN AIRCRAFT DESIGN , ICAS 2006-7.2.4 |
6. Systems, Subsystems and Equipments |
CONTINUOUS SIMULATION SUPPORT
DURING THE DEVELOPMENT PROCESS OF A FUEL CELL SYSTEM ON BOARD OF CONVENTIONAL
AIRCRAFT , ICAS 2006-7.3.2 |
6. Systems, Subsystems and Equipments |
CONTROLLABLE STUDY OF ELECTRO-RHEOLOGICAL
FLUID APPLIED TO LANDING GEAR BUMPER , ICAS 2006-7.11.1 |
6. Systems, Subsystems and Equipments |
ELECTRICAL ROTATING MACHINES
AND POWER ELECTRONICS FOR NEW AIRCRAFT EQUIPMENT SYSTEMS , ICAS 2006-7.1.2 |
6. Systems, Subsystems and Equipments |
ELECTRICALLY POWERED ICE PROTECTION
SYSTEMS FOR MALE UAVS – REQUIREMENTS AND INTEGRATION CHALLENGES ,
ICAS 2006-7.3.3 |
6. Systems, Subsystems and Equipments |
ELECTRIFICATION OF THE ENVIRONMENTAL
CONTROL SYSTEM , ICAS 2006-7.7.1 |
6. Systems, Subsystems and Equipments |
ENVIRONMENTAL CHALLENGE TO AIRBORNE
ELECTRONIC EQUIPMENT MAINTENANCE , ICAS 2006-P6.1 |
6. Systems, Subsystems and Equipments |
FAULT- TOLERANT PROCEDURES FOR
AIR DATA ELABORATION , ICAS 2006-7.9.4 |
6. Systems, Subsystems and Equipments |
FORMULATION AND IMPLEMENTATION
OF AN AIRCRAFT – SYSTEM – SUBSYSTEM INTERRELATIONSHIP MODEL FOR TECHNOLOGY
EVALUATION , ICAS 2006-7.10.2 |
6. Systems, Subsystems and Equipments |
FUEL CELL SYSTEMS FOR AERONAUTIC
APPLICATIONS: A CLEAN WAY FROM KEROSENE TO ENERGY , ICAS 2006-7.3.1 |
6. Systems, Subsystems and Equipments |
GENERATOR POWER OPTIMISATION
FOR A MORE-ELECTRIC AIRCRAFT BY USE OF A VIRTUAL IRON BIRD ,
ICAS 2006-7.5.1 |
6. Systems, Subsystems and Equipments |
HIGH POWER PIEZOELECTRIC MOTOR
FOR BRAKE ACTUATOR- PIBRAC PROJECT , ICAS 2006-7.3.4 |
6. Systems, Subsystems and Equipments |
HIGH SPEED OPTICAL FIBER TRANSMISSION
TECHNOLOGY FOR AVIONICS APPLICATIONS , ICAS2006-7.9S |
6. Systems, Subsystems and Equipments |
INITIAL TEST RESULTS FOR THE
FAN SHAFT DRIVEN GENERATOR , ICAS2006-7.1S |
6. Systems, Subsystems and Equipments |
LABINAL CURRENT WORK TOWARDS THE MORE ELECTRICAL AIRCRAFT
THROUGH THE POA EUROPEAN PROGRAMME, ICAS2006-7.5S |
6. Systems, Subsystems and Equipments |
LATEST DEVELOPMENTS IN LANDING GEARS, ICAS 2006-7.8.1 INVITED: |
6. Systems, Subsystems and Equipments |
METHODS FOR THE DESIGN OF ENERGY
EFFICIENT HIGH-SPEED AEROSPACE VEHICLES , ICAS 2006-7.10.1 |
6. Systems, Subsystems and Equipments |
MIXED CONVECTION IN A FULL SCALE
AIRCRAFT CABIN MOCK-UP , ICAS 2006-7.6.3 |
6. Systems, Subsystems and Equipments |
MODEL-BASED DIAGNOSIS STUDIES
OF COMPLEX FLUID MECHANICAL AIRCRAFT SYSTEMS , ICAS2006-7.10S |
6. Systems, Subsystems and Equipments |
ON-BOARD WIND MEASUREMENT SYSTEM
BASED ON MINIATURIZED NAVIGATION SENSORS , ICAS 2006-7.9.3 |
6. Systems, Subsystems and Equipments |
OPTIMIZATION OF A SPUR GEAR PROFILE FOR MINIMUM TRANSMISSION
ERROR OF A GEAR SET USING GENETIC ALGORITHM, ICAS2006-7.10S |
6. Systems, Subsystems and Equipments |
PASSENGER ACCEPTABILITY ASSESSMENT
MODEL-METHODOLOGY FOR FUTURE CUSTOMER-ORIENTATED AIRCRAFT CABIN DESIGN
, ICAS 2006-7.6.1 |
6. Systems, Subsystems and Equipments |
POWER BY WIRE, AN OPPORTUNITY?, ICAS 2006-7.2.2 |
6. Systems, Subsystems and Equipments |
REAL-TIME HARDWARE-IN-THE-LOOP
SIMULATION OF FLY-BY-WIRE FLIGHT CONTROL SYSTEMS ,
ICAS 2006-7.10.4 |
6. Systems, Subsystems and Equipments |
SIMULATION AND ANALYSIS OF A
NEW HIGH POWER DENSITY GENERATOR , ICAS2006-7.5S |
6. Systems, Subsystems and Equipments |
SIMULATION OF FLUID MECHANICAL
AIRCRAFT SYSTEMS FROM CONCEPT EVALUATION TO QUALIFICATION TESTS ,
ICAS 2006-7.10.3 |
6. Systems, Subsystems and Equipments |
SIMULATION OF LANDING GEAR DYNAMICS
USING FLEXIBLE MULTI-BODY METHODS , ICAS 2006-7.8.3 |
6. Systems, Subsystems and Equipments |
SIMULATION WITH MODELICA FOR
A DYNAMIC REPRESENTATION OF AN AIRCRAFT CABIN CLIMATE FOR COMFORT-IMPROVED
CLIMATE CONTROL , ICAS 2006-7.6.2 |
6. Systems, Subsystems and Equipments |
SMALL-SIGNAL STABILITY STUDIES
OF 270V DC POWER SYSTEM FOR MORE ELECTRIC AIRCRAFT EMPLOYING SWITCHED
RELUCTANCE GENERATOR TECHNOLOGY , ICAS 2006-7.5.3 |
6. Systems, Subsystems and Equipments |
SUBSYSTEM DESIGN AND INTEGRATION
FOR THE MORE ELECTRIC AIRCRAFT , ICAS 2006-7.2.3 INVITED: |
6. Systems, Subsystems and Equipments |
SUMMARY OF THE EUROPEAN POWER
OPTIMISED AIRCRAFT (POA) PROJECT , ICAS 2006-7.2.1 |
6. Systems, Subsystems and Equipments |
THE A380 FLIGHT CONTROL ELECTROHYDROSTATIC
ACTUATORS, ACHIEVEMENTS AND LESSONS LEARNT , ICAS 2006-7.4.1 |
6. Systems, Subsystems and Equipments |
THE DESIGN OF A SERIES OF ELECTROTHERMAL
ICE PROTECTION SYSTEMS , ICAS 2006-P6.4 |
6. Systems, Subsystems and Equipments |
THE DEVELOPMENT OF A ROBUST AIRCRAFT ANTI-SKID CONTROLLER
UTILISING MU-SLIP GRADIENT CONTROL, ICAS 2006-7.11.2 |
6. Systems, Subsystems and Equipments |
THE NEED FOR A MORE EFFICIENT ALTERNATIVE TO THE ENGINE
BLEED AIR OPERATED WING ICE PROTECTION SYSTEM, ICAS2006-7.7S |
6. Systems, Subsystems and Equipments |
THE USE OF A HYBRID ACTUATION PACKAGE FOR IMPROVED EFFICIENCY
IN ELECTRICALLY POWERED FLIGHT ACTUATION, ICAS 2006-7.4.2 |
6. Systems, Subsystems and Equipments |
TOWARD A FIPA COMPLIANT MULTI-AGENT
REAL-TIME ARCHITECTURE FOR INTEGRATED MODULAR AVIONICS , ICAS 2006-7.9.2 |
6. Systems, Subsystems and Equipments |
TRANSIENT SIMULATION OF A DIRECT-EVAPORATING
CO2 COOLING SYSTEM FOR AN AIRCRAFT , ICAS 2006-7.7.4 |
6. Systems, Subsystems and Equipments |
ULTIMATE POWER OPTIMIZING FOR
A ‘STAND ALONE’ LANDING GEAR SYSTEM OF MORE ELECTRIC AIRCRAFT (MEA)
, ICAS 2006-7.8.2 |
6. Systems, Subsystems and Equipments |
A 3D KNOWLEDGE-BASED
ROUTER FOR WIRING IN AEROSPACE VEHICLES , ICAS 2006-9.3.4 |
7. Systems Engineering an Supply Chain |
AGEFORMABLE PANELS FOR COMMERCIAL
AIRCRAFT , ICAS 2006-9.1.3 |
7. Systems Engineering an Supply Chain |
AN ALGORITHMIC MORPHOLOGY MATRIX
FOR AIRCRAFT FUEL SYSTEM CONCEPTUAL DESIGN , ICAS 2006-9.2.2 |
7. Systems Engineering an Supply Chain |
COMPUTATIONAL DESIGN PROCESS
MODELLING , ICAS 2006-9.2.3 |
7. Systems Engineering an Supply Chain |
EVIDENCE OF LEAN ENGINEERING
IN AIRCRAFT PROGRAMS , ICAS 2006-9.4.1 |
7. Systems Engineering an Supply Chain |
FINDING THE REAL VALUE OF ADAPTABLE
VEHICLE CONFIGURATIONS IN AN UNCERTAIN WORLD , ICAS 2006-9.4.4 |
7. Systems Engineering an Supply Chain |
INFUSION TECHNOLOGY FOR AUTOMATED
PRODUCTION OF HIGH PERFORMANCE CFRP-PARTS , ICAS 2006-9.1.2 |
7. Systems Engineering an Supply Chain |
KNOWLEDGE ENABLED PROCESS ENGINEERING-
REVOLUTION OR ADAPTATION , ICAS 2006-9.3.1 |
7. Systems Engineering an Supply Chain |
MANUFACTURING CHALLENGES AND
EXPERIENCES FROM A380, ICAS 2006-9.1.1 INVITED: |
7. Systems Engineering an Supply Chain |
METHODOLOGY FOR THE DESIGN AND
EVALUATION OF WING LEADING EDGE AND TRAILING EDGE DEVICES ,
ICAS 2006-9.2.1 |
7. Systems Engineering an Supply Chain |
METHODS FOR ENGINEERING CHANGE
PROPAGATION ANALYSIS , ICAS 2006-9.3.3 |
7. Systems Engineering an Supply Chain |
RELATIVE LIFE-CYCLE-COST ESTIMATION
OF FUTURE SPACE TRANSPORTATION SYSTEMS AT CONCEPTUAL DESIGN PHASE
,
ICAS 2006-9.4.3 |
7. Systems Engineering an Supply Chain |
SCENARIO-BASED DESIGN COMPETITIVENESS
EXPLORATION WITH SYSTEM DYNAMICS , ICAS 2006-9.4.2 |
7. Systems Engineering an Supply Chain |
THE RESEARCH ON AIRCRAFT RDT&E
COST BASED ON GRAY CORRELATION ANALYSIS THEORY AND EQUALATION-ENGINEERING-VALUE-RATE
, ICAS 2006-9.4.5 |
7. Systems Engineering an Supply Chain |
TOP DOWN CAD MODELING METHODOLOGY
FOR LOW PRESSURE TURBINE DESIGN , ICAS2006-9.2S |
7. Systems Engineering an Supply Chain |
TOWARDS ROBUST ORDER PROCESSING
THROUGH QUALITY INTELLIGENCE , ICAS 2006-9.3.2 |
7. Systems Engineering an Supply Chain |
TRANSFER OF ADVANCED ASAAC SW
TECHNOLOGY ONTO THE EUROFIGHTER/TYPHOON , ICAS 2006-9.2.4 |
7. Systems Engineering an Supply Chain |
USING VIRTUAL ASSEMBLY TECHNOLOGY
TO DESIGN AND DEVELOP THE ARJ21 BUSINESS JET BASE ON CATIA V5 AND
ENOVIA VPM , ICAS 2006-P7.1 |
7. Systems Engineering an Supply Chain |
"FILE
AND FLY"- PROCEDURES AND TECHNIQUES FOR INTEGRATION OF UAVS
IN CONTROLLED AIRSPACE , ICAS 2006-8.4.1 |
8. Air Transport System Efficiency |
4D TRAJECTORY MANAGEMENT IN THE
EXTENDED TMA: COUPLING AMAN AND 4D FMS FOR OPTIMIZED APPROACH TRAJECTORIES
, ICAS 2006-8.8.2 |
8. Air Transport System Efficiency |
A DECISION SUPPORT SYSTEM FOR
HELICOPTER EMERGENCY MEDICAL SERVICE OPERATIONS , ICAS 2006-8.3.2 |
8. Air Transport System Efficiency |
AIRCRAFT PARAMETER AND PROCEDURE
DRIVEN SIMULATION OF AIRPORT AIRSIDE OPERATIONS , ICAS 2006-8.8.1 |
8. Air Transport System Efficiency |
AIRCRAFT WAKE VORTEX SCENARIOS
SIMULATION PACKAGE- WAKESCENE , ICAS 2006-8.6.3 |
8. Air Transport System Efficiency |
AN AGENT-BASED MODEL FOR ANALYZING
CONTROL POLICIES AND THE DYNAMIC SERVICE-TIME PERFORMANCE OF A CAPACITY-CONSTRAINED
AIR TRAFFIC MANAGEMENT FACILITY , ICAS 2006-8.4.2 |
8. Air Transport System Efficiency |
AUTOMATED CONFLCIT RESOLUTION
FOR AIR TRAFFIC CONTROL , ICAS 2006-8.2.1 |
8. Air Transport System Efficiency |
CHANGES IN AIRPORT TERMINAL DESIGN, ICAS 2006-P8.3 |
8. Air Transport System Efficiency |
CONTRIBUTION TO THE OPERATIONAL
EVALUATION OF EGNOS AS AN AERONAUTICAL NAVIGATION SYSTEM ,
ICAS 2006-8.2.3 |
8. Air Transport System Efficiency |
DEVELOPMENT PROBLEMS OF THE VILNIUS
AND KAUNAS AIRPORTS , ICAS2006-8.5S |
8. Air Transport System Efficiency |
EFFICIENCY DRIVEN BY JOINT OBJECTIVES:
A NEW WAY TO ORGANIZE THE AIR TRAFFIC MANAGEMENT , ICAS 2006-8.2.2 |
8. Air Transport System Efficiency |
EMMA- EUROPEAN AIRPORT MOVEMENT
MANAGEMENT BY A-SMGCS- A CONTRIBUTION TO THE VISION 2020 , ICAS 2006-8.5.3 |
8. Air Transport System Efficiency |
ESTIMATION OF DAILY UNSCHEDULED
LINE MAINTENANCE EVENTS IN CIVIL AVIATION , ICAS2006-8.3S |
8. Air Transport System Efficiency |
FUTURE DEVELOPMENTS IN ATM- EUROPÉ, ICAS 2006-8.7.1 INVITED: |
8. Air Transport System Efficiency |
FUTURE DEVELOPMENTS IN ATM- USA, ICAS 2006-8.7.2 INVITED: |
8. Air Transport System Efficiency |
FUTURE DEVELOPMENTS IN ATM- JAPAN , ICAS 2006-8.7.3 INVITED: |
8. Air Transport System Efficiency |
HUMAN FACTORS CONSIDERATIONS
FOR AREA NAVIGATION DEPARTURE AND ARRIVAL PROCEDURES ,
ICAS 2006-8.2.4 |
8. Air Transport System Efficiency |
IMAGE PROCESSING TECHNOLOGY OF
FLIR-BASED ENHANCED VISION SYSTEM , ICAS 2006-P8.2 |
8. Air Transport System Efficiency |
IMPACT OF INDIVIDUAL AND DYNAMIC
WAKE VORTEX SEPARATIONS ON AIRPORT CAPACITY , ICAS 2006-8.6.2 |
8. Air Transport System Efficiency |
INCREASING RUNWAY CAPACITY USING
GENETIC ALGORITHMS AND ENHANCED HEURISTICS , ICAS 2006-8.5.2 |
8. Air Transport System Efficiency |
INTERMODAL INTEGRATION OF LARGE
VOLUME AIR CARGO , ICAS2006-8.5S |
8. Air Transport System Efficiency |
KNOWLEDGE MANAGEMENT CONCEPTS
FOR AIR TRANSPORT SYSTEMS ARCHITECTING , ICAS 2006-8.4.5 |
8. Air Transport System Efficiency |
LASER LIGHT LANDING SYSTEM (LS3)
, ICAS 2006-P8.1 |
8. Air Transport System Efficiency |
MODELS AND PROCEDURES FOR THE
ASSESSMENT OF FUTURE MAINTENANCE TECHNOLOGIES FOR NEXT-GENERATION
AIRLINERS WITHIN THE FUZZY FRONT END OF THE INNOVATION PROCESS , ICAS 2006-8.3.4 |
8. Air Transport System Efficiency |
MONTE CARLO ANALYSIS OF AIRPORT
THROUGHPUT AND TRAFFIC DELAYS USING SELF SEPARATION PROCEDURES ,
ICAS 2006-8.8.3 |
8. Air Transport System Efficiency |
OPERATIONAL FEASIBILITY OF TRAFFIC SYNCHRONISATION IN
CENTRAL EUROPE- RESULTS , ICAS 2006-8.4.3 |
8. Air Transport System Efficiency |
PAVE: ASSISTANCE SYSTEM TO SUPPORT
PILOTS FOR IFR ROTORCRAFT AIRPORT OPERATIONS , ICAS 2006-8.3.1 |
8. Air Transport System Efficiency |
PERSPECTIVES OF AIR TRAFFIC MANAGEMENT
SYSTEM IN RUSSIA , ICAS 2006-8.7.4 INVITED: |
8. Air Transport System Efficiency |
POINT-TO-POINT! VALIDATION OF
THE SMALL AIRCRAFT TRANSPORTATION SYSTEM HIGHER VOLUME OPERATIONS
CONCEPT , ICAS 2006-8.4.4 |
8. Air Transport System Efficiency |
POTENTIAL FOR TRANSPORT EFFICIENCY
IMPROVEMENTS OF AVIATION TRANSPORTATION SYSTEMS , ICAS2006-8.2S |
8. Air Transport System Efficiency |
PROSPECTS FOR HEAD- AND CROSSWIND
DEPENDENT AIRCRAFT SEPARATIONS IN THE CONTEXT OF WAKE VORTEX SAFETY
AND AIRPORT CAPACITY, APPLICATION TO SCHIPHOL AIRPORT , ICAS 2006-8.6.1 |
8. Air Transport System Efficiency |
REAL-TIME AIRCRAFT NOISE PREDICTION
FOR TRAJECTORY BASED ARRIVAL MANAGERS , ICAS 2006-8.11.1 |
8. Air Transport System Efficiency |
REAL-TIME SIMULATION STUDIES
CONCERNING THE OPERATIONAL ASPECTS OF TWO LANDING THRESHOLDS ON ONE
RUNWAY AT FRANKFURT/M , ICAS 2006-8.11.2 |
8. Air Transport System Efficiency |
SNOWFLAKE- DESIGNING AND ORGANISING
A WINTER EXERCISE FOR AMSTERDAM AIRPORT SCHIPHOL , ICAS 2006-8.11.3 |
8. Air Transport System Efficiency |
SPADE: SUPPORTING PLATFORM FOR
AIRPORT DECISION-MAKING AND EFFICIENCY ANALYSIS , ICAS 2006-8.5.1 |
8. Air Transport System Efficiency |
SUMMARY OF NOCTARN RESEARCH PROJECT
, ICAS 2006-8.3.3 |
8. Air Transport System Efficiency |
SYSTEM-OF-SYSTEMS SIMULATION
FOR ANALYZING THE EVOLUTION OF AIR TRANSPORTATION , ICAS 2006-8.7.5 |
8. Air Transport System Efficiency |
AIRBUS FLY-BY-WIRE:
A PROCESS TOWARD TOTAL DEPENDABILITY , ICAS 2006-9.9.1 |
9. Safety and Security |
AIRCRAFT SECURITY : EVOLUTION OF COCKPIT RESOURCE MANAGEMENT
& COCKPIT VIDEO TRANSMISSION, ICAS2006-9.10S |
9. Safety and Security |
AIRPORT SAFETY MANAGEMENT SYSTEM
FOR THE FUTURE , ICAS 2006-10.9.4 |
9. Safety and Security |
AUTOMATIC GUIDANCE FOR TRAFFIC AVOIDANCE- APFD TCAS
MODE,
ICAS 2006-9.9.2 |
9. Safety and Security |
CONCEPTS FOR ENERGY ABSORBING
SUPPORT STRUCTURES AND APPROPRIATE MATERIALS , ICAS 2006-9.6.4 |
9. Safety and Security |
CONFLICT AND SEPARATION SYMBOLS
IN CDTI FOR SMALL AIRCRAFT OPERATION , ICAS 2006-9.10.5 |
9. Safety and Security |
DETERMINATION OF SMOKE QUANTITIES
TO BE USED FOR SMOKE DETECTION PERFORMANCE GROUND AND FLIGHT TESTS
,
ICAS 2006-9.8.2 |
9. Safety and Security |
DEVELOPEMENT OF A PRODUCTION
ORGANIZATION EXPOSITION SCHEME TAKING INTO ACCOUNT EN9100 REQUIREMENTS
, ICAS 2006-P9.2 |
9. Safety and Security |
DEVELOPMENT OF A METHOD FOR CRM
SKILLS MEASUREMENT , ICAS 2006-9.7.4 |
9. Safety and Security |
DEVELOPMENT OF HELICOPTER SAFETY
DEVICES , ICAS2006-9.6S |
9. Safety and Security |
ELECTRONIC SYSTEM FOR DEACTIVATION
OF CLOCK-ACTIVATED BOMBS WITH THE HELP OF LIQUID NITROGEN ,
ICAS 2006-P9.3 |
9. Safety and Security |
ENHANCEMENTS OF FLIGHT MANAGEMENT
SYSTEM WITH INTEROPERABILITY , ICAS 2006-P9.5 |
9. Safety and Security |
ENTROPY METHOD OF RELIABILITY
ASSESSMENT FOR AIRCRAFT SYSTEMS , ICAS2006-8.1S |
9. Safety and Security |
EVALUATION ON FLIGHT MANAGEMENT
SKILL OF JET AIRLINER PILOTS- A CASE OF GO-AROUND- , ICAS 2006-9.10.4 |
9. Safety and Security |
EVS BASED APPROACH PROCEDURES:
IR IMAGE ANALYSIS AND IMAGE FUSION TO SUPPORT PILOTS IN LOW VISIBILITY
, ICAS2006-9.9S |
9. Safety and Security |
FLEET USAGE MONITORING IS ESSENTIAL
IN IMPROVING AGING U.S. ARMY HELICOPTER RELIABILITY AND MAINTAINABILITY
, ICAS 2006-8.1.1 |
9. Safety and Security |
FULL-SCALE CRASH TEST OF A CIVIL
HELICOPTER AT JAXA , ICAS 2006-9.6.1 |
9. Safety and Security |
HEAD-UP GUIDANCE SYSTEM MODEL
2100 AND HUMAN-MACHINE INTERACTION , ICAS 2006-9.10.1 |
9. Safety and Security |
HELICOPTER SUBFLOOR-INTEGRATED
FUEL-TANK CRASHWORTHINESS , ICAS 2006-9.6.3 |
9. Safety and Security |
HYDROGEN TECHNOLOGY – READY FOR
TAKE-OFF – HYDROGEN APPLICATIONS IN AEROSPACE INDUSTRY , ICAS 2006-P9.4 |
9. Safety and Security |
IMPACT OF WORKPLACE ENVIRONMENT
ON HEALTH AND COMFORT OF FLIGHT ATTENDANTS AND PILOTS- RESULTS FROM
THE EU PROJECT HEACE , ICAS 2006-9.7.1 |
9. Safety and Security |
IMPROVED WEATHER INFORMATION
FOR COCKPIT AND TOWER , ICAS 2006-9.5.2 |
9. Safety and Security |
INCORPORATING DATA LINK MESSAGING
INTO A MULTI-FUNCTION DISPLAY FOR GENERAL AVIATION AIRCRAFT ,
ICAS 2006-9.9.3 |
9. Safety and Security |
INCREASING AVIATION SAFETY BY
ASSESSING ENGLISH LANGUAGE PROFICIENCY AMONG AVIATION POFESSIONALS
,
ICAS2006-9.7S |
9. Safety and Security |
INTRODUCTION OF DUAL THRESHOLD OPERATION IN FRANKFURT/MAIN-
EVALUATION OF HUMAN-FACTORS FROM THE PILOT’S PERSPECTIVE, ICAS2006-9.7S |
9. Safety and Security |
NEW TECHNOLOGIES FOR REDUCING
AVIATION WEATHER-RELATED ACCIDENTS , ICAS 2006-9.5.1 |
9. Safety and Security |
ON AN ABSOLUTE SAFETY CRITERION
FOR THE PROBABILITY OF THE COLLISION BETWEEN AIRCRAFT , ICAS 2006-9.5.3 |
9. Safety and Security |
ON THE CONNECTION BETWEEN PILOT'S
PERFORMANCE AND INCREASING COMPLEXITY OF FLIGHT SIMULATION SYSTEMS
, ICAS 2006-9.7.2 |
9. Safety and Security |
ON THE VALIDATION OF HELICOPTER
FLIGHT SIMULATORS OPERATING IN EMERGENCY PROCEDURES , ICAS 2006-8.1.3 |
9. Safety and Security |
PEDESTRIAN DYNAMICS IN AIRPORT
TERMINALS CONSIDERING EMERGENCY CASES , ICAS 2006-10.9.3 |
9. Safety and Security |
PILOT EVALUATION OF A TAKE-OFF
MONITOR DISPLAY , ICAS 2006-9.9.4 |
9. Safety and Security |
PILOT GAZE AND PERFORMANCE WITH RESPECT TO SITUATION
AWARENESS,
ICAS 2006-9.7.3 |
9. Safety and Security |
PILOTING COGNITIVE PERFORMANCE: THE EUCALEPIC EFFECT
IN THE COCKPIT, ICAS 2006-9.7.5 |
9. Safety and Security |
PILOT-IN-THE-LOOP EVALUATION
OF NEXT GENERATION WEATHER RADAR DISPLAYS , ICAS 2006-9.10.3 |
9. Safety and Security |
RELIABILITY ASSESSMENT OF COMPLEX ELECTRO-MECHANICAL
SYSTEMS TAKING INTO ACCOUNT SYSTEM-STRUCTURE INTERACTION., ICAS 2006-8.1.2 |
9. Safety and Security |
RESEARCH ON RELIABILITY GROWTH
TECHNOLOGY OF ELECTROMECHANICAL-HYDRAULIC SYSTEM , ICAS 2006-P9.6 |
9. Safety and Security |
RISK ASSESSMENT OF NEWLY PROPOSED
SYSTEMS TO IMPROVE IN-FLIGHT SECURITY , ICAS 2006-10.9.2 |
9. Safety and Security |
SAFEE: SECURITY OF AIRCRAFT IN THE FUTURE EUROPEAN ENVIRONMENT,
ICAS 2006-10.9.1 |
9. Safety and Security |
SAFETY FOR LITTLE TRAVELERS- CHILD RESTRAINT SYSTEMS-
GETTING SAFELY OFF THE GROUND, ICAS2006-9.8S |
9. Safety and Security |
SELECTION OF PARAMETERS IN FIXED-DURATION
RELIABILITY QUALIFICATION TEST SCHEME , ICAS 2006-P9.1 |
9. Safety and Security |
STUDIES ON THE PERFORMANCE OF
SMOKE DETECTORS AND THEIR HOUSING IN AN AIRCRAFT CARGO COMPARTMENT
ENVIRONMENT , ICAS 2006-9.8.1 |
9. Safety and Security |
THE RESEARCH DEVELOPMENT OF MAN-MACHINE-ENVIRONMENT
SYSTEM ENGINEERING TECHNOLOGY IN THE AIRCRAFT DESIGN OF CHINA , ICAS 2006-9.10.2 |
9. Safety and Security |
USING DETECTION INDICES (DIS)
TO DETECT AIR VEHICLE CHARACTERISTIC CHANGES FOR HUMS APPLICATION
,
ICAS 2006-9.8.3 |
9. Safety and Security |
VIRTUAL CO-PILOT SYSTEM IN GENERAL AVIATION, ICAS2006-9.9S |
9. Safety and Security |
A STRATEGY
TOWARDS SUSTAINABLE DEVELOPMENT OF UK AVIATION , ICAS 2006-5.10.1 INVITED: |
10. Challenge of the Environment |
ADVANCED LINER COOLING NUMERICAL
ANALYSIS FOR LOW EMISSION COMBUSTORS , ICAS 2006-5.8.3 |
10. Challenge of the Environment |
AERONET III “AIRCRAFT EMISSIONS AND REDUCTION TECHNOLOGIES”,
A EUROPEAN FUNDED COORDINATION ACTION, ICAS 2006-P10.1 |
10. Challenge of the Environment |
AN ALGEBRAIC APPROACH TO AGGREGATE SUBJECT RESPONSE
IN AIRCRAFT NOISE MANAGEMENT, ICAS2006-5.10S |
10. Challenge of the Environment |
AVIATION ENVIRONMENTAL POLICY
ASSESSMENT THROUGH DYNAMIC SIMULATION , ICAS 2006-5.10.3 |
10. Challenge of the Environment |
BENCHMARKING AND VALIDATION OF PREDICTION METHODS FOR
LOW NOISE AIRCRAFT DESIGN, ICAS 2006-5.7.4 |
10. Challenge of the Environment |
CLIMATE CHANGE IMPACT OF AIR
TRAFFIC , ICAS 2006-5.9.1 |
10. Challenge of the Environment |
CONTRAIL AND CIRRUS CLOUD AVOIDANCE
, ICAS2006-5.9S |
10. Challenge of the Environment |
DEVELOPING QUIETER AIRCRAFT, ICAS 2006-5.7.2 |
10. Challenge of the Environment |
DEVELOPMENT OF SILENT AIRFRAME
CONCEPTS AND INNOVATIVE CYCLE PROPULSION SYSTEMS FOR REDUCTION IN
AIRCRAFT NOISE , ICAS 2006-5.7.3 |
10. Challenge of the Environment |
DO AIRCRAFT BLACK CARBON EMISSIONS
AFFECT CIRRUS CLOUDS ON THE GLOBAL SCALE ? , ICAS2006-5.9S |
10. Challenge of the Environment |
ECATS- A EUROPEAN NETWORK OF EXCELLENCE FOR AN ENVIRONMENTAL
AIR TRANSPORT SYSTEM, ICAS 2006-P10.2 |
10. Challenge of the Environment |
HIGH-RESOLUTION WEATHER FORECAST
EXPERIMENTS ON THE EARTH SIMULATOR: CONNECTIONS TO AERONAUTICS ,
ICAS 2006-5.9.3 INVITED: |
10. Challenge of the Environment |
HOLISTIC APPROACH FOR ENVIRONMENTALLY
FRIENDLY AIRCRAFT DESIGN , ICAS 2006-5.10.5 |
10. Challenge of the Environment |
OPERATIONAL ISSUES ASSOCIATED WITH AN ADAPTIVE CONTRAIL
AVOIDANCE POLICY, ICAS 2006-5.9.4 |
10. Challenge of the Environment |
ORGANISATION OF EUROPEAN AERONAUTIC
ULTRA-LOW NOX COMBUSTION RESEARCH , ICAS 2006-5.8.1 |
10. Challenge of the Environment |
REDUCING THE ENVIRONMENTAL IMPACT
OF AVIATION BY USING SUSTAINABLE DEVELOPMENT INDICATORS ,
ICAS 2006-5.10.4 |
10. Challenge of the Environment |
SUSTAINING AVIATION GROWTH- MEETING
THE ENVIRONMENTAL CHALLENGES , ICAS 2006-5.10.2 INVITED: |
10. Challenge of the Environment |
THE BOEING QUIET TECHNOLOGY DEMONSTRATOR
PROGRAM , ICAS 2006-5.7.1 INVITED: |
10. Challenge of the Environment |
USING FAA’S SAGE MODEL TO CONDUCT
GLOBAL INVENTORIES AND TO ASSESS ROUTE-SPECIFIC VARIABILITY IN AVIATION
FUEL BURN, EMISSIONS AND COSTS , ICAS 2006-5.9.2 |
10. Challenge of the Environment |