| AUTHOR |
SESSION |
TITLE |
LINK |
| ABISROR, A. |
ICAS 2002-6.2.3 |
COST AND CYCLES REDUCTION BASED ON MANUFACTURING PROCESS SIMULATION |
 |
| ABOTT, E.A. |
ICAS 2002-6.10.1 |
MULTIDISCIPLINARY DESIGN OPTIMISATION FOR EMBEDDED SENSOR DESIGNS |
|
| ACAR, H. |
ICAS 2002-R1 |
THE EFFECT OF THE ANGLE OF THE INCLINED FLAT PLATE ON THE DEFLEXION OF
A PLANE WALL JET |
|
| ACCARDO, A.F. |
ICAS 2002-4.10.5 |
DEVELOPMENT APPROACH AND TESTING OF AN UNMANNED AERIAL VEHICLE |
|
| ACHAIBOU, A.K. |
ICAS 2002-7.5.2 |
TRAJECTORY GENERATION AND DISPLAY FOR RELATIVE NAVIGATION OF TRANSPORTATION
AIRCRAFT |
|
| AFAGH, F.F. |
ICAS 2002-R2 |
INTEGRATED ACTIVE FIBRES IN VIBRATION CONTROL OF HELICOPTER BLADES |
|
| ALI, N. |
ICAS 2002-1.1.4 |
CONCEPTUAL AIRCRAFT DESIGN - A GENETIC SEARCH AND OPTIMIZATION APPROACH |
|
| ALIGHANBARI, H. |
ICAS 2002-4.1.3 |
NONLINEAR AEROELASTIC SIGNAL ANALYSIS OF AN AIRFOIL-AILERON COMBINATION |
|
| ALLEN, C B |
ICAS 2002-4.1.1 |
NUMERICAL SIMULATION OF ACTIVE CONTROL OF TRANSONIC FLUTTER |
|
| ALLEN, C. |
ICAS 2002-R3 |
AN UNSTEADY FLOW-SOLVER WITH ALGEBRAIC GRID MOTION FOR AEROELASTIC SIMULATIONS |
|
| AMATO, M. |
ICAS 2002-2.1.1 |
CFD ANALYSIS OF LOW SPEED AND CRUISE APIAN CONFIGURATION POWERED BY HIGH
SPEED PROPELLERS |
|
| AMATO, M. |
ICAS 2002-2.4.4 |
VALIDATION OF CIRA FLOW SOLVER ZEN FOR SCT LOW-SPEED HIGH-LIFT COMPUTATIONS |
|
| AMEYE, O. |
ICAS 2002-7.6.1 |
EXPANDED ACCOMMODATION ANALYSIS AND RAPID PROTOTYPING
TECHNIQUE FOR THE DESIGN OF A CREW STATION COCKPIT |
|
| AMIRYANTS, G. |
ICAS 2002-4.3.2 |
REVIEW AND OUTLOOK ON ACTIVE AND PASSIVE AEROELASTIC DESIGN CONCEPTS FOR
FUTURE AIRCRAFT |
|
| AMIRYANTS, G.A. |
ICAS 2002-4.6.1 (I.L.) |
INVESTIGATIONS OF AIRSHIP AEROELASTICITY |
|
| AMPRIKIDIS, M. |
ICAS 2002-4.3.2 |
REVIEW AND OUTLOOK ON ACTIVE AND PASSIVE AEROELASTIC DESIGN CONCEPTS FOR
FUTURE AIRCRAFT |
|
| AMRAOUI, Y. |
ICAS 2002-8.3.5 |
LASER VIBROMETRY BASED DETECTIONS OF DELAMINATIONS IN AEROSPACE COMPOSITES |
|
| ANDERLE, P. |
ICAS 2002-3.6.3 |
USING OF THE LOW TURBULENCE WIND TUNNEL FOR INVESTIGATION OF THREE-DIMENSIONAL
UNSTEADY FLOW IN CURVED CHANNELS |
|
| ANDERSSON, K. |
ICAS 2002-5.3.2 |
AERODYNAMIC AND FLIGHT DYNAMIC REAL-TIME ANALYSIS DURING SPIN AND CAREFREE
MANEUVERING TESTS OF THE SAAB JAS39 GRIPEN |
|
| ANGHILERI, M. |
ICAS 2002-4.6.3 |
RIGID BODIES IMPACTS ON WATER SURFACE. NUMERICAL AND EXPERIMENTAL ACTIVITY |
|
| ARIZONO, H. |
ICAS 2002-4.2.3 |
APPLICATION OF AEROELASTIC TAILORING TO ARROW WING CONFIGURATION |
|
| ARMSTRONG, C.G. |
ICAS 2002-3.2.1 |
EFFICIENT NON-LINEAR MODELLING OF FUSELAGE PANELS |
|
| ASAKO, T. |
ICAS 2002-5.9.2 |
CONCEPTUAL DESIGN OF AIRCRAFT ENGINE USING MULTIDISCIPLINARY DESIGN OPTIMIZATION
TECHNIQUE |
|
| ASGHAR, H. |
ICAS 2002-6.8.1 |
OPTICAL DESIGN OF TWO FIELD OF VIEW INFRA-RED OBJECTIVE IN 3-5 MICRON
BAND FOR FOCAL PLANE ARRAY DETECTOR |
|
| ASIM, M. |
ICAS 2002-1.3.4 |
DESIGNING AND DEVELOPMENT OF UNMANNED AERIAL VEHICLE |
|
| ASTABURUAGA, M.F. |
ICAS 2002-7.11.3 |
ENVIRONMENTAL, ECONOMICAL AND TECHNICAL ASPECTS OF A CRYOPLANE IN THE
PRELIMINARY DESIGN PHASE |
|
| ASTARITA, T. |
ICAS 2002-3.6.4 |
SPIRAL VORTICES DETECTION ON A ROTATING DISK |
|
| ATLI, V. |
ICAS 2002-R15 |
INTERACTION OF TWO PARALLEL RECTANGULAR JETS |
|
| AURITI, L. |
ICAS 2002-7.8.3 |
KING AIR 350 FLIGHT-TEST DATA GATHERING AND LEVEL-D SIMULATOR AERODYNAMIC
MODEL DEVELOPMENT |
|
| AVANZINI, G. |
ICAS 2002-5.6.3 |
DESIGN OF A SHIPBOARD RECOVERY SYSTEM FOR A SHROUDED-FAN UAV |
|
| AVERARDO, M.A. |
ICAS 2002-2.1.1 |
CFD ANALYSIS OF LOW SPEED AND CRUISE APIAN CONFIGURATION POWERED BY HIGH
SPEED PROPELLERS |
|
| AZEVEDO, J.L.F. |
ICAS 2002-2.6.3 |
THREE-DIMENSIONAL VISCOUS FLOW SIMULATIONS OVER A COMPLETE SATELLITE LAUNCHER
USING OVERSET GRIDS |
|
| AZEVEDO, J.L.F. |
ICAS 2002-R7 |
NORMAL FORCE CALCULATIONS FOR ROCKET-LIKE CONFIGURATIONS |
|
| BAI, J. |
ICAS 2002-2.7.4 |
TRANSONIC AILERON BUZZ BOUNDARY PREDICTION USING HOPF-BIFURCATION ANALYSIS
METHOD |
|
| BALABUYEV, P.V. |
ICAS 2002-P1 |
AN-70 STOL AIRCRAFT CHARACTERISTICS AT HIGH ANGLES OF ATTACK AND TAKEOFF
AND LANDING CHARACTERISTICS |
|
| BALAS, G. |
ICAS 2002-5.4.1 (I.L.) |
LINEAR, PARAMETER-VARYING CONTROL AND ITS APPLICATION TO AEROSPACE SYSTEMS |
|
| BANASZEK, J. |
ICAS 2002-6.6.2 |
DEVELOPING A NEW FLAP FOR A LIGHT UTILITY TRANSPORT AIRPLANE |
|
| BAO, G. |
ICAS 2002-6.10.2 |
ACTIVE FAULT-TOLERANT CONTROL SYSTEM DESIGN FOR A TWO-ENGINE BLEED AIR
SYSTEM OF AN AIRCRAFT |
|
| BARBOSA, L.C.P. |
ICAS 2002-6.8.2 |
A MISSION PLANNER AND NAVIGATION SYSTEM FOR THE ARARA PROJECT |
|
| BARLOW, D.A. |
ICAS 2002-R62 |
CALCULATING THE COST OF A CARBON FIBRE COMPOSITE STRUCTURE FROM WITHIN
A FINITE ELEMENT MODEL |
|
| BAROLLO, J. |
ICAS 2002-P12 |
EXPERIMENTAL ASSESSMENT AND ANALYSIS OF THE CREW WORKLOAD |
|
| BARON, A. |
ICAS 2002-5.2.3 |
THEORETICAL, EXPERIMENTAL AND IN-FLIGHT SPIN INVESTIGATIONS FOR AN EXECUTIVE
LIGHT AIRPLANE |
|
| BARRERA, L. |
ICAS 2002-2.5.3 |
ADVANCED NUMERICAL SIMULATIONS ON STRUCTURED GRIDS FOR TRANSPORT AIRCRAFT,
USING AN EFFICIENT OBJECT ORIENTED SOLVER |
|
| BASSI, P. |
ICAS 2002-4.10.5 |
DEVELOPMENT APPROACH AND TESTING OF AN UNMANNED AERIAL VEHICLE |
|
| BASSO, E. |
ICAS 2002-2.6.3 |
THREE-DIMENSIONAL VISCOUS FLOW SIMULATIONS OVER A COMPLETE SATELLITE LAUNCHER
USING OVERSET GRIDS |
|
| BAUER, S.X.S. |
ICAS 2002-1.10.2 |
LOW-SONIC-BOOM DESIGN METHODOLOGIES FOR FUTURE SUPERSONIC AIRCRAFT |
|
| BAUER, S.X.S. |
ICAS 2002-2.10.2 |
SIMULATION OF FLOWS WITH PASSIVE POROSITY |
|
| BAUER, S.X.S. |
ICAS 2002-8.7.1 (I.L.) |
AERODYNAMIC DESIGN OPPORTUNITIES FOR FUTURE SUPERSONIC AIRCRAFT |
|
| BAUMGARTNER, R. |
ICAS 2002-8.9.4 |
LOCKHEED MARTIN’S HISTORY OF SUPERSONIC AIRCRAFT |
|
| BAYANDOR, J. |
ICAS 2002-R4 |
PARAMETRIC BASED AERODYNAMIC DESIGN OF PERFORMANCE ENHANCING BLADING SYSTEMS |
|
| BECKER, K. |
ICAS 2002-1.10.5 |
MEGAFLOW - A NUMERICAL FLOW SIMULATION TOOL FOR TRANSPORT AIRCRAFT DESIGN |
|
| BEHDINAN, K |
ICAS 2002-1.1.4 |
CONCEPTUAL AIRCRAFT DESIGN - A GENETIC SEARCH AND OPTIMIZATION APPROACH |
|
| BELLASTRADA, C. |
ICAS 2002-3.8.2 |
INVESTIGATIONS ON THE TURBULENT WAKE VORTEX FLOW OF LARGE TRANSPORT AIRCRAFT |
|
| BENARD, E. |
ICAS 2002-2.8.3 |
PREDICTION OF LAMINAR-TO-TURBULENT TRANSITION IN INCOMPRESSIBLE FLOW PAST
3-D CAVITY |
|
| BENGIN, A. |
ICAS 2002-R12 |
NUMERICAL MODEL OF SINGLE MAIN ROTOR HELICOPTER DYNAMICS |
|
| BENGIN, A. |
ICAS 2002-R5 |
AN ALGORITHM FOR THE CALCULATION OF AERODYNAMIC WING-PROPELLER INTERACTION |
|
| BENGIN, A. |
ICAS 2002-R71 |
ADAPTIVE MODELING AND OPTIMIZATION OF PILOT HELMETS FOR DIFFERENT KINDS
OF IMPACTS WITH HARD OBSTACLES |
|
| BENMEDDOUR, A. |
ICAS 2002-2.6.2 |
IAR STORES CLEARANCE CFD APPROACH:
FROM DEVELOPMENT TO AUTOMATED ENGINEERING TOOL |
|
| BENOIT, C.H. |
ICAS 2002-2.5.3 |
ADVANCED NUMERICAL SIMULATIONS ON STRUCTURED GRIDS FOR TRANSPORT AIRCRAFT,
USING AN EFFICIENT OBJECT ORIENTED SOLVER |
|
| BENTAMY, A. |
ICAS 2002-1.2.3 |
WING SHAPE OPTIMIZATION USING A CONSTRAINED NURBS SURFACE GEOMETRICAL
REPRESENTATION |
|
| BERAN, P.S. |
ICAS 2002-4.4.5 |
INVESTIGATION OF SHOCK-INDUCED LCO OF A WING/STORE CONFIGURATIONUSING
THE TRANSONIC SMALL DISTURBANCE METHOD |
|
| BERES, W. |
ICAS 2002-5.8.3 |
STRESS INTENSITY FACTOR CALCULATIONS FOR CRACKS EMANATING FROM BOLT HOLES
IN A JET ENGINE COMPRESSOR DISC |
|
| BERGE, D. |
ICAS 2002-8.4.5 |
COMPARISON OF TWO CFD-BASED METHODS FOR THE PREDICTION OF THE TONE-NOISE
GENERATED BY THE FAN-OGV INTERACTION CASE |
|
| BERTON, E. |
ICAS 2002-R6 |
CENTRIFUGAL AND 3D EFFECTS ON THE NEAR TIP SECTION OF ROTATING BLADE |
|
| BESSERT, N. |
ICAS 2002-4.6.1 (I.L.) |
INVESTIGATIONS OF AIRSHIP AEROELASTICITY |
|
| BEYERS, M. E. |
ICAS 2002-3.10.4 |
OVERVIEW OF ROTARY FLOW VISUALIZATION RESULTS ON THE F/A-18 AIRCRAFT |
|
| BEYERS, M.E. |
ICAS 2002-3.6.1 |
FLOW MECHANISMS ACTIVE IN WING ROCK OF COMBAT AIRCRAFT |
|
| BIGARELLI, E.D.V. |
ICAS 2002-R7 |
NORMAL FORCE CALCULATIONS FOR ROCKET-LIKE CONFIGURATIONS |
|
| BIL, C. |
ICAS 2002-5.6.2 |
AN AUTONOMOUS CONTROL TECHNIQUE FOR LAUNCHING SHIP BASED UNMANNED AIR
VEHICLES (UAVS) IN EXTREME CONDITIONS |
|
| BISAGNI, C. |
ICAS 2002-4.9.1 |
EXPERIMENTAL BUCKLING TESTS AND NUMERICAL ANALYSES OF STIFFENED CYLINDRICAL
SHELLS IN COMPOSITE MATERIALS |
|
| BLAIR, K. |
ICAS 2002-7.8.3 |
KING AIR 350 FLIGHT-TEST DATA GATHERING AND LEVEL-D SIMULATOR AERODYNAMIC
MODEL DEVELOPMENT |
|
| BLOM, H.A.P. |
ICAS 2002-R76 |
HUMAN COGNITION PERFORMANCE MODEL BASED EVALUATION OF SAFE SPACING IN
AIR TRAFFIC |
|
| BLUME, S. |
ICAS 2002-3.7.2 |
EXPERIMENTAL INVESTIGATIONS ON THE ADAPTATION ACCURACY OF ADAPTIVE SLOTS
IN WIND TUNNEL TEST SECTION WALLS |
|
| BOCCADORO, C. |
ICAS 2002-8.9.3 |
NORTHRUP GRUMANN’S FLIGHT TEST ON SONIC BOOM MITIGATION |
|
| BOERMANS, L.M.M. |
ICAS 2002-2.9.4 |
SIMPLIFIED DESIGN METHOD FOR A SYMMETRICAL WING-BODY FAIRING |
|
| BOGDANOV, O.K |
ICAS 2002-P1 |
AN-70 STOL AIRCRAFT CHARACTERISTICS AT HIGH ANGLES OF ATTACK AND TAKEOFF
AND LANDING CHARACTERISTICS |
|
| BOGUSLAVSKY, S. |
ICAS 2002-R9 |
MOTOR CASE FOR ROCKET TRAJECTORY CORRECTION SYSTEM |
|
| BOLSUNOVSKY, A. |
ICAS 2002-1.5.2 |
THE DOLPHIN: A NEW 100-SEAT AIRCRAFT IN LIFTING-FUSELAGE LAYOUT |
|
| BOOGERS, J.A.M. |
ICAS 2002-8.6.1 |
PATCH REPAIR OF CRACKS IN THE UPPER LONGERON OF AN F-16 AIRCRAFT OF THE
ROYAL NETHERLANDS AIR FORCE (RNLAF) |
|
| BORELLO, L. |
ICAS 2002-R77 |
PROPOSALS AND COMPARATIVE EVALUATION OF SYNTHETIC NONLINEAR MODELS IN
FLIGHT CONTROLS SIMULATION |
|
| BORGGAARD, J. |
ICAS 2002-1.9.4 |
SENSITIVITY AND UNCERTAINTY ANALYSIS OF AERODYNAMIC FLOWS |
|
| BOUHEMHEM, D. |
ICAS 2002-1.4.5 |
A CONFIGURABLE FRAMEWORK FOR MULTIDISCIPLINARY ANALYSIS INTEGRATION AND
MANAGEMENT |
|
| BOURDIN, P. |
ICAS 2002-2.2.3 |
NUMERICAL PREDICTIONS OF WING-TIP EFFECTS ON LIFT-INDUCED DRAG |
|
| BOUSQUET, J.M. |
ICAS 2002-2.7.2 |
PREDICTION OF UNSTEADY FLOWS AROUND ROTATING BLADES |
|
| BOZDOGAN, K. |
ICAS 2002-6.5.4 |
FOSTERING INNOVATION ACROSS SUPPLIER NETWORKS CHALLENGES AND OPPORTUNITIES |
|
| BRAGIN, |
ICAS 2002-8.8.2 (St) |
DOWNWASH FLOW INVESTIGATIONS FOR PASSANGER AIRPLANE |
|
| BRANDI, V. |
ICAS 2002-2.4.4 |
VALIDATION OF CIRA FLOW SOLVER ZEN FOR SCT LOW-SPEED HIGH-LIFT COMPUTATIONS |
|
| BRANDT, J. |
ICAS 2002-6.3.4 |
NEW APPROACHES IN TEXTILE AND IMPREGNATION TECHNOLOGIES FOR THE COST EFFECTIVE
MANUFACTURING OF CFRP AEROSPACE COMPONENTS |
|
| BRAY, D. |
ICAS 2002-1.6.3 |
SUPERSONIC BUSINESS JET AIRCRAFT DESIGN |
|
| BREITSAMTER, C. |
ICAS 2002-3.8.2 |
INVESTIGATIONS ON THE TURBULENT WAKE VORTEX FLOW OF LARGE TRANSPORT AIRCRAFT |
|
| BRENNER, M.J. |
ICAS 2002-4.4.2 |
AEROSERVOELASTIC ROBUST MODEL DEVELOPMENT FROM FLIGHT DATA |
|
| BROICHHAUSEN, G. |
ICAS 2002-4.7.3 |
CLEAN : THE EUROPEAN ENVIRONMENTALLY FRIENDLY ENGINE DEMONSTRATOR |
|
| BROICHHAUSEN, K. |
ICAS 2002-5.10.2 |
COMPRESSOR TECHNOLOGY FROM INNOVATION TO ECONOMICS |
|
| BROUGHTON, C. |
ICAS 2002-3.7.5 |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE FLOWFIELD IN A BLOWDOWN
WIND TUNNEL |
|
| BUCHHOLZ, S. |
ICAS 2002-3.10.3 |
TESTING OF A DASH 8 Q400 IN THE NASA AMES 80x120' WIND TUNNEL |
|
| BUSACKER, T. |
ICAS 2002-7.7.1 |
A CONTRIBUTION TO PROACTIVELY PLANNING AND MANAGING AIRPORT GROUND TRAFFIC
USING A STOCHASTIC MODELLING APPROACH |
|
| BUSCHMANN, M. |
ICAS 2002-5.5.2 |
MODELING OF THE NONLINEAR DYNAMIC BEHAVIOR OF A MICRO-AERIAL-VEHICLE (MAV)
IN AN ENVIRONMENT OF A TURBULENT ATMOSPHERE |
|
| CAI, H.J. |
ICAS 2002-3.10.4 |
OVERVIEW OF ROTARY FLOW VISUALIZATION RESULTS ON THE F/A-18 AIRCRAFT |
|
| CALISKAN, T. |
ICAS 2002-R65 |
ACTIVE VIBRATION CONTROL OF A SMART PLATE |
|
| CAMPOS, L.M.B.C. |
ICAS 2002-2.9.1 |
ON TRANSMISSION OF SOUND ACROSS A NON ISOTHERMAL BOUNDARY LAYER |
|
| CAMPOS, L.M.B.C. |
ICAS 2002-8.4.4 |
ON THE ACOUSTIC MODES IN A CYLINDRICAL NOZZLE WITH AN ARBITRARY IMPEDANCE
DISTRIBUTION |
|
| CAMPOS, L.M.B.C. |
ICAS 2002-R71 |
ON WAKE VORTEX RESPONSE FOR SEVERAL COMBINATIONS
OF LEADING AND FOLLOWING AIRCRAFT |
|
| CAMPOS, L.M.B.C. |
ICAS 2002-R8 |
ON THE CALCULATION OF COLLISION PROBABILITIES AS AN ASSURANCE OF SAFE
SEPARATION BETWEEN AIRCRAFT |
|
| CANDEL, S |
ICAS 2002-8.7.2 (I.L) |
A RESEARCH INITIATIVE ON THE SUPERSONIC AIRCRAFT |
|
| CARDONE, G. |
ICAS 2002-3.6.4 |
SPIRAL VORTICES DETECTION ON A ROTATING DISK |
|
| CARLOMAGNO, G.M. |
ICAS 2002-3.6.4 |
SPIRAL VORTICES DETECTION ON A ROTATING DISK |
|
| CARRERAS, C. |
ICAS 2002-8.8.1 (St) |
THE CASE FOR A PRACTICAL SMALL SUPERSONIC TRANSPORT |
|
| CARUANA, D. |
ICAS 2002-3.9.5 |
MATHEMATICAL MODELLING AND ACTIVE CONTROL OF OSCILLATORS. APPLICATION
TO BUFFET AND TO COMPRESSOR SURGE. |
|
| CASALIS, G. |
ICAS 2002-2.9.2 |
RELATIONSHIP BETWEEN INSTABILITY WAVES AND NOISE OF LOW SUPERSONIC JETS |
|
| CATALANO, F.M. |
ICAS 2002-3.10.2 |
THE EFFECT OF WING TIP BLOWING ON THE VORTEX DRAG |
|
| CATALANO, F.M. |
ICAS 2002-P2 |
VISCOUS AND WAVE DRAG OPTIMIZATION FOR A TRANSPORT AIRCRAFT MISSION ADAPTIVE
WING |
|
| CATALANO, P. |
ICAS 2002-2.4.4 |
VALIDATION OF CIRA FLOW SOLVER ZEN FOR SCT LOW-SPEED HIGH-LIFT COMPUTATIONS |
|
| CENKO, A. |
ICAS 2002-2.6.1 |
EVALUATION OF THE CAPABILITIES OF CFD TO PREDICT STORE TRAJECTORIES FROM
ATTACK AIRCRAFT |
|
| CERUTI, A. |
ICAS 2002-5.7.5 |
A FUZZY LOGIC AUTOPILOT DEVELOPMENT FOR A LIGHT TWIN ENGINE AIRCRAFT IN
THE APPROACH FLIGHT CONDITION |
|
| CHABLE, S. |
ICAS 2002-5.4.2 |
ROBUSTIFICATION OF AN H2 AUTOPILOT FOR FLEXIBLE AIRCRAFT BY SELF-SCHEDULING
BASED ON MULTI-MODEL EIGENSTRUCTURE ASSIGNMENT |
|
| CHANG, W-Y. |
ICAS 2002-R35 |
THE DEVELOPMENT OF A LOW COST AUTONOMOUS UAV SYSTEM |
|
| CHARLES, G. |
ICAS 2002-5.3.1 |
FEEDBACK STABILISED BIFURCATION TAILORING APPLIED TO AIRCRAFT MODELS |
|
| CHARLES, J.L. |
ICAS 2002-7.1.1 |
ASSESMENT OF EXPLICIT F.E. CAPABILITIES FOR FULL SCALE COUPLED FLUID/STRUCTURE
AIRCRAFT DITCHING SIMULATIONS |
|
| CHEN, N. |
ICAS 2002-2.1.4 |
A RAPID NUMERICAL METHOD FOR 3D AERO DYNAMICS DESIGN OF COMPRESSOR BLADE
ROW (APPLICATION TO A LOW SPEED EXPERIMENTAL MULTI-IDENTICAL-STAGE COMPRESSOR
DESIGN) |
|
| CHEN, S. |
ICAS 2002-1.1.3 |
EVALUATION OF THREE DECOMPOSITION MDO ALGORITHMS |
|
| CHEN, S. |
ICAS 2002-2.11.1 |
OPTIMIZATIONS OF AIRFOIL AND WING USING GENETIC ALGORITHM |
|
| CHEN, W.R. |
ICAS 2002-R67 |
THIRTY YEARS OF RETROGRESSION AND REAGING |
|
| CHEN, Z. |
ICAS 2002-5.7.3 |
DETECTION AND ISOLATION OF CONTROL SURFACE EFFECTIVENESS LOSS IN AIRCRAFT
BY USING FILTER BANK APPROACH |
|
| CHENG, C-Z. |
ICAS 2002-R24 |
EXPERIMENTAL STUDY OF TURBULENT WAKE FLOW DEVELOPMENT BEHIND A FINITE
WING WITH HIGH ANGLE OF ATTACKS |
|
| CHEREVATSKY, A. |
ICAS 2002-R9 |
MOTOR CASE FOR ROCKET TRAJECTORY CORRECTION SYSTEM |
|
| CHERNYSHEV, |
ICAS 2002-8.1.2 |
HYBRID TWO-LEVEL GENETIC OPTIMIZATION ALGORITHM WITH DIFFERENT FIDELITY
MODELS FOR AERODYNAMIC DESIGN PROBLEMS |
|
| CHESTER, D.H. |
ICAS 2002-R10 |
PRE-STRESSED SYMMETRIC COMPOSITE BEAMS IN AIRCRAFT - ANALYSIS AND DESIGN
IMPLICATIONS |
|
| CHIAPPA, C. |
ICAS 2002-5.4.2 |
ROBUSTIFICATION OF AN H2 AUTOPILOT FOR FLEXIBLE AIRCRAFT BY SELF-SCHEDULING
BASED ON MULTI-MODEL EIGENSTRUCTURE ASSIGNMENT |
|
| CHIESA, S. |
ICAS 2002-1.6.2 |
ASSESSMENT OF THE FEASIBILITY OF INNOVATIVE REUSABLE LAUNCHERS |
|
| CHISHOLM, T. |
ICAS 2002-1.9.3 |
A FULLY COUPLED NEWTON-KRYLOV SOLVER FOR TURBULENT AERODYNAMIC FLOWS |
|
| CHOI, N.C. |
ICAS 2002-5.2.2 |
A LOW COST FLIGHT TEST INSTRUMENTATION PACKAGE FOR LIGHT AIRPLANES |
|
| CHOI, N.S. |
ICAS 2002-6.6.2 |
DEVELOPING A NEW FLAP FOR A LIGHT UTILITY TRANSPORT AIRPLANE |
|
| CHOUDHARI, M. |
ICAS 2002-1.7.5 |
STOCHASTIC MODELING OF LAMINAR-TURBULENT TRANSITION |
|
| CHOUDHARI, M.M. |
ICAS 2002-8.4.1 (I.L.) |
FLOW AND NOISE CONTROL: TOWARD A CLOSER LINKAGE |
|
| CHRISTIANSEN, L.E. |
ICAS 2002-4.1.4 |
ON THE NONLINEAR DYNAMICS APPROACH OF MODELING THE BIFURCATION FOR TRANSONIC
LIMIT CYCLE FLUTTER |
|
| CHRISTNER, B. |
ICAS 2002-6.3.1 |
DEVELOPMENT AND TESTING OF FRICTION STIR WELDING (FSW) AS A JOINING METHOD
FOR PRIMARY AIRCRAFT STRUCTURE |
|
| CLAYTON, G. |
ICAS 2002-R62 |
CALCULATING THE COST OF A CARBON FIBRE COMPOSITE STRUCTURE FROM WITHIN
A FINITE ELEMENT MODEL |
|
| COIMBRA, F.M. |
ICAS 2002-3.10.2 |
THE EFFECT OF WING TIP BLOWING ON THE VORTEX DRAG |
|
| COIRO, D.P. |
ICAS 2002-5.2.1 |
FLYING QUALITIES ANALYSIS OF A THREE SURFACES AIRCRAFT MODEL |
|
| COLWELL, J.L. |
ICAS 2002-5.6.4 |
REAL TIME SHIP MOTION CRITERIA FOR MARITIME HELICOPTER OPERATIONS |
|
| CONSTANT, G. |
ICAS 2002-5.4.2 |
ROBUSTIFICATION OF AN H2 AUTOPILOT FOR FLEXIBLE AIRCRAFT BY SELF-SCHEDULING
BASED ON MULTI-MODEL EIGENSTRUCTURE ASSIGNMENT |
|
| COOPER, J. |
ICAS 2002-4.3.2 |
REVIEW AND OUTLOOK ON ACTIVE AND PASSIVE AEROELASTIC DESIGN CONCEPTS FOR
FUTURE AIRCRAFT |
|
| COOPER, R.K |
ICAS 2002-2.8.3 |
PREDICTION OF LAMINAR-TO-TURBULENT TRANSITION IN INCOMPRESSIBLE FLOW PAST
3-D CAVITY |
|
| CORDISCO, P. |
ICAS 2002-4.9.1 |
EXPERIMENTAL BUCKLING TESTS AND NUMERICAL ANALYSES OF STIFFENED CYLINDRICAL
SHELLS IN COMPOSITE MATERIALS |
|
| CORREGE, M. |
ICAS 2002-3.9.5 |
MATHEMATICAL MODELLING AND ACTIVE CONTROL OF OSCILLATORS. APPLICATION
TO BUFFET AND TO COMPRESSOR SURGE. |
|
| CORRIVEAU, D. |
ICAS 2002-5.11.4 |
IMPACT OF FLOW QUALITY IN TRANSONIC CASCADE WIND TUNNELS: MEASUREMENTS
IN AN HP TURBINE CASCADE |
|
| CROSS, A.G.T. |
ICAS 2002-2.9.3 |
DESIGN METHOD FOR PROBLEMS INVOLVING SHOCK BOUNDARY-LAYER INTERACTION |
|
| CRUMP, M.R. |
ICAS 2002-5.6.2 |
AN AUTONOMOUS CONTROL TECHNIQUE FOR LAUNCHING SHIP BASED UNMANNED AIR
VEHICLES (UAVS) IN EXTREME CONDITIONS |
|
| CUI, D. |
ICAS 2002-6.1.4 |
PROCESS MODELING AND REENGINEERING ON AIRCRAFT PRODUCT LIFECYCLE |
|
| CUI, D. |
ICAS 2002-R11 |
BEND/TWIST COUPLING EFFECTS FOR UNSYMMETRICAL & UNBALANCED LAMINATE USED
IN AIRCRAFT WING STRUCTURE ANALYSIS |
|
| CUI, D. |
ICAS 2002-R42 |
FATIGUE LIFE PREDICTION OF 3-D PROBLEMS BY DAMAGE MECHANICS WITH SPECTRUM
LOADING |
|
| CUI, M. |
ICAS 2002-7.5.3 |
THE HIERARCHICAL AVAILABILITY ANALYSIS FOR FLIGHT CONTROL SYSTEM |
|
| CUI, Y.Y. |
ICAS 2002-P3 |
ANALYSIS OF PREVENTIVE MAINTENANCE PROGRAM IMPROVEMENT FOR IN-SERVICE
AIRCRAFT |
|
| CURTIS, P.T. |
ICAS 2002-3.1.2 |
FAILURE PREDICTION OF STRINGER STIFFENED COMPOSITE PANELS WITH IMPACT
DAMAGE UNDER UNIAXIAL COMPRESSION |
|
| CVETKOVIC, D. |
ICAS 2002-R12 |
NUMERICAL MODEL OF SINGLE MAIN ROTOR HELICOPTER DYNAMICS |
|
| CVETKOVIC, D. |
ICAS 2002-R13 |
ALGORITHM FOR AUTOMATIC GENERATION OF THE TECHNICAL DOCUMENTATION OF HELICOPTER
COMPOSITE TAIL ROTOR BLADES IN TIS |
|
| CVETKOVIC, D. |
ICAS 2002-R71 |
ADAPTIVE MODELING AND OPTIMIZATION OF PILOT HELMETS FOR DIFFERENT KINDS
OF IMPACTS WITH HARD OBSTACLES |
|
| DABAYEH, A. |
ICAS 2002-R14 |
EXTENSION OF REPAIR LIFETIME FOR THE CP140 BY COLD WORKING OF FATIGUED
HOLES |
|
| DAOUK, M. |
ICAS 2002-8.8.1 (St) |
THE CASE FOR A PRACTICAL SMALL SUPERSONIC TRANSPORT |
|
| DARBON, P. |
ICAS 2002-7.7.2 |
AN OBJECT-ORIENTED METHODOLOGY FOR MANAGING THE COMPLEXITY OF ATM SYSTEMS |
|
| DAVARI, A.R. |
ICAS 2002-2.10.5 |
FLOW CONTROL OVER THE WING OF A FIGHTER-TYPE CONFIGURATION USING BOUNDARY
LAYER SUCTION |
|
| DAYAN, H. |
ICAS 2002-R9 |
MOTOR CASE FOR ROCKET TRAJECTORY CORRECTION SYSTEM |
|
| DE DIVITIIS, N. |
ICAS 2002-P4 |
AERODYNAMIC MODELING AND PERFORMANCE ANALYSIS OF A SHROUDED-FAN UNMANNED
AERIAL VEHICLE |
|
| DE JONGE, A. |
ICAS 2002-4.8.2 |
PLASTICITY CORRECTION FACTORS FOR BUCKLING OF FLAT RECTANGULAR GLARE PLATES
LOADED IN COMPRESSION OR SHEAR |
|
| DE MARCO, A. |
ICAS 2002-5.2.1 |
FLYING QUALITIES ANALYSIS OF A THREE SURFACES AIRCRAFT MODEL |
|
| DE MATTEIS, G. |
ICAS 2002-5.6.3 |
DESIGN OF A SHIPBOARD RECOVERY SYSTEM FOR A SHROUDED-FAN UAV |
|
| DE RANGO, S. |
ICAS 2002-6.6.2 |
DEVELOPING A NEW FLAP FOR A LIGHT UTILITY TRANSPORT AIRPLANE |
|
| DE RUITER, A. |
ICAS 2002-R37 |
CONTROL INTEGRATION PROCESS IN AIRCRAFT SYSTEMS DEVELOPMENT |
|
| DELAURENTIS, D. |
ICAS 2002-1.1.1 |
A PROBABILISTIC METHODOLOGY FOR THE TREATMENT OF SYSTEM-OF-SYSTEMS PROBLEMS
AND APPLICATION TO FUTURE AIR TRANSPORTATION ARCHITECTURES |
|
| DELOISON, D. |
ICAS 2002-6.2.3 |
COST AND CYCLES REDUCTION BASED ON MANUFACTURING PROCESS SIMULATION |
|
| DEMENTYEV, A.D. |
ICAS 2002-3.4.5 |
SERVICE LIFE OF A TITANIUM MAIN WING BOX FOR SECOND GENERATION SUPERSONIC
COMMERCIAL TRANSPORT |
|
| DEY, D. |
ICAS 2002-7.7.3 |
A COST/BENEFIT ANALYSIS OF AFAS FUNCTIONALITIES FOR A FUTURE ATM-SYSTEM |
|
| D'HENIN, E. |
ICAS 2002-4.6.1 (I.L.) |
INVESTIGATIONS OF AIRSHIP AEROELASTICITY |
|
| DI BERNARDO, M. |
ICAS 2002-5.3.1 |
FEEDBACK STABILISED BIFURCATION TAILORING APPLIED TO AIRCRAFT MODELS |
|
| DI CICCA, G.M. |
ICAS 2002-2.10.4 |
DPIV INVESTIGATION OF A TURBULENT BOUNDARY LAYER MANIPULATED BY TRANSVERSAL
WALL OSCILLATIONS |
|
| DI CICCA, G.M. |
ICAS 2002-3.9.4 |
FLOW CONTROL DOWNSTREAM OF A BACKWARD FACING STEP: A DPIV STUDY |
|
| DILLINGH, J.E. |
ICAS 2002-8.2.4 |
WAVE DEVELOPMENT ON THIN LAYERS OF ANTI-ICING FLUID |
|
| DING, L. |
ICAS 2002-P3 |
ANALYSIS OF PREVENTIVE MAINTENANCE PROGRAM IMPROVEMENT FOR IN-SERVICE
AIRCRAFT |
|
| DIRKS, G.A. |
ICAS 2002-6.5.3 |
BALANCING ACCURACY OF CALCULATIONS AND PROBABILITY OF ASSUMPTIONS IN THE
TECHNOLOGY INTEGRATION |
|
| DIRMEIER, S. |
ICAS 2002-1.2.2 |
DEVELOPMENT AND INTEGRATION OF A NEW HIGH PERFORMANCE WINGTIP DEVICE FOR
TRANSONIC AIRCRAFT |
|
| DJAYAPERTAPA, L. |
ICAS 2002-4.1.1 |
NUMERICAL SIMULATION OF ACTIVE CONTROL OF TRANSONIC FLUTTER |
|
| DJOJODIHARDJO, H. |
ICAS 2002-2.11.2 |
COMPUTATIONAL STUDY OF THE AERODYNAMIC CHARACTERISTICS OF AXI-SYMMETRIC
BODIES IN TRANSONIC FLOW |
|
| DOERRIES, R. |
ICAS 2002-7.10.1 |
DEVELOPMENT OF APPROACH PROCEDURE DESIGN CRITERIA FOR SYSTEMS BASED ON
GLOBAL NAVIGATION SATELLITE SYSTEM (GNSS) WITH GROUND BASED AUGMENTATION
SYSTEM (GBAS) |
|
| DOMB, M. |
ICAS 2002-3.2.2 |
NONLINEAR BUCKLING PREDICTIONS OF CURVED PANELS UNDER COMBINED
COMPRESSION AND SHEAR LOADING |
|
| DOWNEN, T. |
ICAS 2002-8.8.1 (St) |
THE CASE FOR A PRACTICAL SMALL SUPERSONIC TRANSPORT |
|
| D™LL, C. |
ICAS 2002-5.4.2 |
ROBUSTIFICATION OF AN H2 AUTOPILOT FOR FLEXIBLE AIRCRAFT BY SELF-SCHEDULING
BASED ON MULTI-MODEL EIGENSTRUCTURE ASSIGNMENT |
|
| DURMU, G. |
ICAS 2002-P6 |
MULTI BLOCK NAVIER STOKES SOLUTIONS OF LOW ASPECT RATIO RECTANGULAR FLAT
WINGS IN COMPRESSIBLE FLOW |
|
| DURMUS, G. |
ICAS 2002-R30 |
MULTI BLOCK NAVIER STOKES SOLUTIONS OF LOW ASPECT RATIO RECTANGULAR FLAT
WINGS IN COMPRESSIBLE FLOW |
|
| DZHAMGAROV, S.I. |
ICAS 2002-1.5.2 |
THE DOLPHIN: A NEW 100-SEAT AIRCRAFT IN LIFTING-FUSELAGE LAYOUT |
|
| EASTEP, F. |
ICAS 2002-4.4.5 |
INVESTIGATION OF SHOCK-INDUCED LCO OF A WING/STORE CONFIGURATIONUSING
THE TRANSONIC SMALL DISTURBANCE METHOD |
|
| EDI, P. |
ICAS 2002-R52 |
THE APPLICATION OF HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER FLAP
AS A FLOW CONTROL ON THE WING FOR REGIONAL AIRCRAFT FAMILY |
|
| EDWARDS, K.L. |
ICAS 2002-5.1.1 |
THE EFFECT OF AIRCRAFT BIASES ON THE DELIVERY OF AN ENHANCED LASER-GUIDED
WEAPON |
|
| EDWARDS, K.L. |
ICAS 2002-5.7.1 |
MINIMISING THE RISK OF COLLATERAL DAMAGE WITH THE KALMAN-LEVY FILTER |
|
| EGGLESTON, B. |
ICAS 2002-4.11.3 (I.L.) |
PIONEERS OF FLIGHT IN CANADA |
|
| EGGLESTON, B. |
ICAS 2002-5.2.2 |
A LOW COST FLIGHT TEST INSTRUMENTATION PACKAGE FOR LIGHT AIRPLANES |
|
| EGGLESTON, B. |
ICAS 2002-6.6.2 |
DEVELOPING A NEW FLAP FOR A LIGHT UTILITY TRANSPORT AIRPLANE |
|
| EKMEDZIC, A. |
ICAS 2002-8.1.3 |
SIMULATION OF TURBULENT AIRFOIL FLOW |
|
| ELLIOTT, G. |
ICAS 2002-3.4.2 |
OPTIMAL DESIGN OF FUSELAGE STRUCTURES |
|
| ELLIOTT, M. |
ICAS 2002-3.7.1 |
HIGH REYNOLDS NUMBER SIMULATION IN A TRANSONIC WIND TUNNEL BY SURFACE
SUCTION |
|
| ELLIS, F. |
ICAS 2002-3.7.5 |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE FLOWFIELD IN A BLOWDOWN
WIND TUNNEL |
|
| EPSTEIN, B. |
ICAS 2002-1.7.4 |
AN ACCURATE MULTIBLOCK ENO DRIVEN NAVIER-STOKES SOLVER FOR COMPLEX AERODYNAMIC
CONFIGURATIONS |
|
| ERDEM, D. |
ICAS 2002-R15 |
INTERACTION OF TWO PARALLEL RECTANGULAR JETS |
|
| ERDEM, M. |
ICAS 2002-8.6.3 |
EB VARESTRAINT TEST METHOD AND AN APPLICATION |
|
| ERICSSON, L. E. |
ICAS 2002-3.6.1 |
FLOW MECHANISMS ACTIVE IN WING ROCK OF COMBAT AIRCRAFT |
|
| EVERDIJ, M.H.C. |
ICAS 2002-7.9.2 |
SAFETY-SEPARATION ASSESSMENT OF SATELLITE-BASED EN-ROUTE ATC VERSUS CONVENTIONAL
EN-ROUTE ATC |
|
| EVERDIJ, M.H.C. |
ICAS 2002-R76 |
HUMAN COGNITION PERFORMANCE MODEL BASED EVALUATION OF SAFE SPACING IN
AIR TRAFFIC |
|
| FAVIER, D. |
ICAS 2002-R6 |
CENTRIFUGAL AND 3D EFFECTS ON THE NEAR TIP SECTION OF ROTATING BLADE |
|
| FEATHERSTON, C.A. |
ICAS 2002-3.4.4 |
MULTILEVEL OPTIMIZATION OF AEROSPACE
AND LIGHTWEIGHT STRUCTURES |
|
| FEJTEK, I. |
ICAS 2002-2.4.5 |
INVERSE DESIGN OF HIGH LIFT SYSTEMS |
|
| FERGUSON, N. |
ICAS 2002-4.10.2 |
AN EVALUATION OF THE PHYSICAL PROPERTIES OF ND:YAG LASER WELDED HIGH
STRENGTH 6000 SERIES ALUMINUM ALLOYS |
|
| FERREIRA, O.D.C.S. |
ICAS 2002-7.3.3 |
ON ICE BLOCKAGE OF VENT TUBES IN THE WING FUEL TANKS OF THE EPSILON AIRCRAFT |
|
| FERSAN, K. |
ICAS 2002-7.5.1 |
AUTOMATIC AIRCRAFT COLLISION AVOIDANCE SYSTEM FOR AIR COMBAT MANEUVERING |
|
| FIELDING, J.P. |
ICAS 2002-R16 |
DEVELOPMENT OF ENVIRONMENTALLY-FRIENDLY TECHNOLOGIES AND CONFIGURATIONS
FOR SUBSONIC JET TRANSPORTS |
|
| FILATYEV, A. |
ICAS 2002-1.4.2 |
MULTIDISCIPLINARY OPTIMIZATION OF AIRCRAFT PARAMETERS BY THE LOCAL DISTRIBUTED
CRITERIA METHOD |
|
| FILSINGER, J. |
ICAS 2002-6.3.4 |
NEW APPROACHES IN TEXTILE AND IMPREGNATION TECHNOLOGIES FOR THE COST EFFECTIVE
MANUFACTURING OF CFRP AEROSPACE COMPONENTS |
|
| FISCHER, B. |
ICAS 2002-5.3.4 (I.L.) |
HIGH ANGLE OF ATTACK APPROACH AND LANDING CONTROL LAW DESIGN FOR THE X-31A |
|
| FISCHER, B. |
ICAS 2002-5.6.1 (I.L.) |
APPLICATION OF ESTOL FLIGHT CONTROL TECH-NOLOGY TO UCAV DESIGN |
|
| FISCHER, M. |
ICAS 2002-3.4.4 |
MULTILEVEL OPTIMIZATION OF AEROSPACE
AND LIGHTWEIGHT STRUCTURES |
|
| FLAMM, J.D. |
ICAS 2002-8.7.1 (I.L.) |
AERODYNAMIC DESIGN OPPORTUNITIES FOR FUTURE SUPERSONIC AIRCRAFT |
|
| FLOHR, P. |
ICAS 2002-5.8.2 |
VORTEX BREAKDOWN CONTROL FOR REDUCED COMBUSTION PRESSURE PULSATIONS |
|
| FLORYAN, J.M. |
ICAS 2002-R17 |
DESIGN OF SURFACE ROUGHNESS FOR PASSIVE FLOW CONTROL |
|
| FOKIN, D. |
ICAS 2002-P14 |
STRUCTURAL CONCEPTS AND AERODYNAMIC DESIGN OF SHOCK CONTROL BUMPS |
|
| FORTIN, F. |
ICAS 2002-2.6.2 |
IAR STORES CLEARANCE CFD APPROACH:
FROM DEVELOPMENT TO AUTOMATED ENGINEERING TOOL |
|
| FORTSON, M.L. |
ICAS 2002-6.1.1 (I.L.) |
JOINT STRIKE FIGHTER (JSF) DEVELOPMENT FOCUSING ON REDUCED LIFECYCLE COSTS |
|
| FRANZ, A, |
ICAS 2002-4.6.1 (I.L.) |
INVESTIGATIONS OF AIRSHIP AEROELASTICITY |
|
| FRICKE, M. |
ICAS 2002-7.10.1 |
DEVELOPMENT OF APPROACH PROCEDURE DESIGN CRITERIA FOR SYSTEMS BASED ON
GLOBAL NAVIGATION SATELLITE SYSTEM (GNSS) WITH GROUND BASED AUGMENTATION
SYSTEM (GBAS) |
|
| FRICKE, M. |
ICAS 2002-7.7.1 |
A CONTRIBUTION TO PROACTIVELY PLANNING AND MANAGING AIRPORT GROUND TRAFFIC
USING A STOCHASTIC MODELLING APPROACH |
|
| FRIEND, M. |
ICAS 2002-6.9.1 (I.L.)+C528 |
INTERNATIONAL COOPERATION IN THE DEVELOPMENT OF NEW TECHNOLOGY FOR COMMERCIAL
TRANSPORTS |
|
| FRINK, N. |
ICAS 2002-2.10.2 |
SIMULATION OF FLOWS WITH PASSIVE POROSITY |
|
| FRULLA, G. |
ICAS 2002-4.10.4 |
BEARING STRENGTH OF BOLTED JOINTS IN CFRP WING FITTINGS |
|
| FU, D.W. |
ICAS 2002-2.5.2 |
RECENT EXAMPLES ON DESIGN AERODYNAMICS FOR TRANSPORT AIRCRAFT |
|
| FUJITA, T. |
ICAS 2002-2.3.1 |
EFFICIENT WING DESIGN FOR COMPLEX AIRCRAFT CONFIGURATION USING CAD, UNSTRUCTURED
CFD AND INVERSE PROBLEMS |
|
| FUJITSUNA, Y. |
ICAS 2002-6.4.2 (I.L.) |
PROGRAM OVERVIEW AND INTERMEDIATE ACHIEVEMENTS OF "RESEARCH AND DEVELOPMENT
OF ENVIRONMENTALLY COMPATIBLE PROPULSION SYSTEM FOR
NEXT-GENERATION SUPERSONIC TRANSPORT(ESPR PROJECT) |
|
| FUKAGAWA, H. |
ICAS 2002-3.4.3 |
THE CFRP SANDWICH PANEL FOR AIRCRAFT NOSE STRUCTURE |
|
| FUNDANGA, B.M.M. |
ICAS 2002-7.3.3 |
ON ICE BLOCKAGE OF VENT TUBES IN THE WING FUEL TANKS OF THE EPSILON AIRCRAFT |
|
| GALLIZIO, M. |
ICAS 2002-8.2.2 |
HYPOTHESIS ON THE ENHANCING OF THE PROBABILITY OF SURVIVAL OF SPACE AND
TRANSATMOSPHERIC VEHICLES IN SPACE DEBRIS AND MICROMETEOROIDS CONTAMINATED
ENVIRONMENT |
|
| GALLIZIO, M. |
ICAS 2002-8.8.3 (St) |
ACCESSIBILITY AND MAINTAINABILITY STUDIES THROUGH DIGITAL HUMANS IN A
DIGITAL MOCK-UP CONTEXT |
|
| GAO, G. |
ICAS 2002-1.9.1 |
SIMULATION OF STATISTICAL MEAN BEHAVIORS AND COHERENT STRUCTURES OF INCOMPRESSIBLE
TURBULENT FLOWS USING UNILATERAL-AVERAGE BASED GOVERNING EQUATIONS |
|
| GAO, J. |
ICAS 2002-P5 |
USING DATA MINING METHOD FOR ANALYZING OTS CAPTURE ZONE |
|
| GARCIA, L. |
ICAS 2002-7.8.2 (I.L.) |
Aging Military Aircraft |
|
| GAZAIX, M. |
ICAS 2002-1.10.3 |
THE elsA OBJECT ORIENTED COMPUTATIONAL TOOL FOR INDUSTRIAL APPLICATIONS |
|
| GENG, W. |
ICAS 2002-5.8.2 |
VORTEX BREAKDOWN CONTROL FOR REDUCED COMBUSTION PRESSURE PULSATIONS |
|
| GENITO, N. |
ICAS 2002-5.2.1 |
FLYING QUALITIES ANALYSIS OF A THREE SURFACES AIRCRAFT MODEL |
|
| GESSLER, A. |
ICAS 2002-6.3.4 |
NEW APPROACHES IN TEXTILE AND IMPREGNATION TECHNOLOGIES FOR THE COST EFFECTIVE
MANUFACTURING OF CFRP AEROSPACE COMPONENTS |
|
| GIBSON, A. |
ICAS 2002-3.2.1 |
EFFICIENT NON-LINEAR MODELLING OF FUSELAGE PANELS |
|
| GIBSON, A. |
ICAS 2002-R18 |
AN INVESTIGATION INTO THE EFFECTS OF EXPERIMENTAL ERRORS ON THE CORRELATION
BETWEEN FEA AND TEST RESULTS FOR A WELDED FUSELAGE PANEL |
|
| GOLIKOV, A.A. |
ICAS 2002-1.4.2 |
MULTIDISCIPLINARY OPTIMIZATION OF AIRCRAFT PARAMETERS BY THE LOCAL DISTRIBUTED
CRITERIA METHOD |
|
| GORAJ, Z. |
ICAS 2002-5.2.3 |
THEORETICAL, EXPERIMENTAL AND IN-FLIGHT SPIN INVESTIGATIONS FOR AN EXECUTIVE
LIGHT AIRPLANE |
|
| GORAJ, Z. |
ICAS 2002-R19 |
EXTREME LOADS OF A TRAINER JET FOLLOWING A SUDDEN DEFLECTION OF CONTROL
SURFACE |
|
| GOTO, N. |
ICAS 2002-5.1.2 |
3D-SIMULATION OF NONLINEAR DYNAMICS FOR A REENTRY VEHICLE |
|
| GOTTMANN, T. |
ICAS 2002-1.4.4 |
CONCEPTUAL DESIGN OPTIMISATION OF A "MALE" CONFIGURATION USING A FLEXIBLE
SCALING TOOL |
|
| GRAHAM, A.D. |
ICAS 2002-0.6 |
THE CANADIAN AND AUSTRALIAN F/A-18 INTERNATIONAL FOLLOW-ON STRUCTURAL
TEST PROJECT |
|
| GRAHAM, G. |
ICAS 2002-0.6 |
THE CANADIAN AND AUSTRALIAN F/A-18 INTERNATIONAL FOLLOW-ON STRUCTURAL
TEST PROJECT |
|
| GRAHAM, M. |
ICAS 2002-5.9.4 |
ADAPTIVE SELECTION OF PARETO OPTIMAL ENGINE TECHNOLOGY SOLUTION SETS |
|
| GRASJO, I. |
ICAS 2002-7.9.3 |
A MODEL FOR SIMULATION OF FLIGHT PASSAGES THROUGH TRAILING TIP VORTICES |
|
| GRECO, P.C. JR. |
ICAS 2002-P2 |
VISCOUS AND WAVE DRAG OPTIMIZATION FOR A TRANSPORT AIRCRAFT MISSION ADAPTIVE
WING |
|
| GREEN, J.E. |
ICAS 2002-3.7.1 |
HIGH REYNOLDS NUMBER SIMULATION IN A TRANSONIC WIND TUNNEL BY SURFACE
SUCTION |
|
| GREEN, J.J. |
|
ICAS ,
THE INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES,
A BRIEF HISTORY |
|
| GREEN, S. |
ICAS 2002-R45 |
TRAJECTORY MODELING ACCURACY FOR AIR TRAFFIC MANAGEMENT DECISION SUPPORT
TOOLS |
|
| GREENWELL, D.I. |
ICAS 2002-R20 |
AN ENGINEERING MODEL OF DELTA WING VORTEX BREAKDOWN |
|
| GRIGORIEV, V.D |
ICAS 2002-4.6.1 (I.L.) |
INVESTIGATIONS OF AIRSHIP AEROELASTICITY |
|
| GRILLO, D. |
ICAS 2002-R40 |
IMPLEMENTATION AND VALIDATION OF THE SPALART-ALLMARAS TURBULENCE MODEL
FOR HIGH SPEED FLOWS |
|
| GROSVENOR, A.D. |
ICAS 2002-1.9.2 |
AN EVALUATION OF SEVERAL LOW-RE TURBULENCE MODELS PART 1- FLAT-PLATE BOUNDARY
LAYER AND AXISYMMETRIC SEPARATING FLOWS |
|
| GRUENEWALD, M. |
ICAS 2002-8.5.3 |
ADVANCED ACTIVE CONCEPTS FOR LOW NOISE ROTORCRAFT |
|
| GUEDRA-DEGEORGES, D. |
ICAS 2002-6.2.3 |
COST AND CYCLES REDUCTION BASED ON MANUFACTURING PROCESS SIMULATION |
|
| GUIBAULT, F. |
ICAS 2002-1.2.3 |
WING SHAPE OPTIMIZATION USING A CONSTRAINED NURBS SURFACE GEOMETRICAL
REPRESENTATION |
|
| GUIBAULT, F. |
ICAS 2002-1.4.5 |
A CONFIGURABLE FRAMEWORK FOR MULTIDISCIPLINARY ANALYSIS INTEGRATION AND
MANAGEMENT |
|
| GUIDI, A. |
ICAS 2002-8.3.1 |
RE-ENTRY MOTION OF AN AXIALSYMMETRIC VEHICLE AND ITS ANALYSIS BASED ON
FLIGHT SIMULATION |
|
| GUINARD, S. |
ICAS 2002-4.9.2 |
INTEGRATED NUMERICAL ANALYSIS FOR COMPOSITE DAMAGE TOLERANCE |
|
| GUNNION, A.J. |
ICAS 2002-3.1.3 |
A LINEAR 3-D FINITE ELEMENT UNIT CELL MODEL FOR FIBRE WAVINESS IN COMPOSITE
MATERIALS |
|
| GUTMARK, E. |
ICAS 2002-5.8.2 |
VORTEX BREAKDOWN CONTROL FOR REDUCED COMBUSTION PRESSURE PULSATIONS |
|
| GUYNN, M.D. |
ICAS 2002-8.5.1 (I.L.) |
NOISE REDUCTION TECHNOLOGY FOR THE 21ST CENTURY |
|
| GUZ, I. |
ICAS 2002-3.1.2 |
FAILURE PREDICTION OF STRINGER STIFFENED COMPOSITE PANELS WITH IMPACT
DAMAGE UNDER UNIAXIAL COMPRESSION |
|
| HACHENBERG, D. |
ICAS 2002-3.1.3 |
A LINEAR 3-D FINITE ELEMENT UNIT CELL MODEL FOR FIBRE WAVINESS IN COMPOSITE
MATERIALS |
|
| HACHENBERG, D. |
ICAS 2002-8.6.2 |
AN APPROACH TO MODELLING AND PREDICTING IMPACT DAMAGE IN COMPOSITE STRUCTURES |
|
| HAHN, K.U. |
ICAS 2002-7.3.2 |
COPING WITH WAKE VORTEX |
|
| HAIYE, L. |
ICAS 2002-R38 |
A SIMPLE AND NONLINEAR AERODYNAMIC MODELING FOR DELTA WITH WITH LEV BREAKDOWN
INVOLVED |
|
| HAJIYEV, CH. |
ICAS 2002-6.8.4 |
ROBUST INTEGRATED INS/RADAR ALTIMETER ACCOUNTING FAULTS AT THE MEASUREMENT
CHANNELS |
|
| HALLOCK, J. |
ICAS 2002-7.9.1 |
CAPACITY AND WAKE VORTICES |
|
| HALSTEAD, D.E. |
ICAS 2002-5.11.3 |
FLOWFIELD UNSTEADINESS AND TURBULENCE IN MULTISTAGE LOW PRESSURE TURBINES |
|
| HAMDANI, H. |
ICAS 2002-R23 |
SEPARATION CONTROL BY ALTERNATING TANGENTIAL BLOWING/SUCTION AT MULTIPLE
SLOTS |
|
| HANADA, T. |
ICAS 2002-5.11.1 |
RESEARCH ON APPLICATION OF CERAMIC TURBINE TO JET ENGINE |
|
| HANFF, E. |
ICAS 2002-3.9.2 |
ENHANCED MANEUVERABILITY BY ACTIVE VORTEX CONTROL WITH MOVEABLE BLOWING
JET |
|
| HANSEN, E. |
ICAS 2002-R21 |
FAST AND ACCURATE SURFACE AND GRID CREATION ON A COMPLETE AIRCRAFT FOR
A CARTESIAN GRID BASED EULER SOLVER |
|
| HANUS, D. |
ICAS 2002-3.6.3 |
USING OF THE LOW TURBULENCE WIND TUNNEL FOR INVESTIGATION OF THREE-DIMENSIONAL
UNSTEADY FLOW IN CURVED CHANNELS |
|
| HARDING, S. |
ICAS 2002-1.6.3 |
SUPERSONIC BUSINESS JET AIRCRAFT DESIGN |
|
| HARMAN, D. |
ICAS 2002-5.4.3 |
ROBUST FLIGHT CONTROL : A REAL TIME SIMULATION INVESTIGATION |
|
| HASEGAWA, H. |
ICAS 2002-2.10.3 |
ACTIVE SEPARATION CONTROL SYSTEM IMPROVED FOR CONTROL TIME AND SUPPRESSION
EFFECT |
|
| HASEGAWA, H. |
ICAS 2002-5.11.1 |
RESEARCH ON APPLICATION OF CERAMIC TURBINE TO JET ENGINE |
|
| HATA, Y. |
ICAS 2002-6.4.2 (I.L.) |
PROGRAM OVERVIEW AND INTERMEDIATE ACHIEVEMENTS OF "RESEARCH AND DEVELOPMENT
OF ENVIRONMENTALLY COMPATIBLE PROPULSION SYSTEM FOR
NEXT-GENERATION SUPERSONIC TRANSPORT(ESPR PROJECT) |
|
| HAUPT, M.C. |
ICAS 2002-1.4.3 |
WITH PUBLIC DOMAIN SOFTWARE TO INTEGRATED DESIGN AND ANALYSIS TOOLS |
|
| HAUSE, T. |
ICAS 2002-3.1.1 |
GEOMETRICALLY LINEAR/NONLINEAR SANDWICH STRUCTURES WITH ANISOTROPIC FACE
SHEETS: THEORY AND BEHAVIOR |
|
| HAYASHI, K. |
ICAS 2002-1.8.2 |
A STUDY ON REDUCTION OF AERODYNAMIC HEATING LOAD BY OPPOSING JET IN HYPERSONIC
FLOW |
|
| HEGEDUS, M.C. |
ICAS 2002-2.3.4 |
LVX - AN INTEGRATED AERODYNAMIC DESIGN AND ANALYSIS METHOD |
|
| HEINRICH, R. |
ICAS 2002-4.6.2 |
FLUID-STRUCTURE COUPLING USING CFD AND MULTIBODY SIMULATION METHODS |
|
| HEINZE, W. |
ICAS 2002-1.4.3 |
WITH PUBLIC DOMAIN SOFTWARE TO INTEGRATED DESIGN AND ANALYSIS TOOLS |
|
| HELLER, G. |
ICAS 2002-1.10.5 |
MEGAFLOW - A NUMERICAL FLOW SIMULATION TOOL FOR TRANSPORT AIRCRAFT DESIGN |
|
| HELLER, G. |
ICAS 2002-1.2.2 |
DEVELOPMENT AND INTEGRATION OF A NEW HIGH PERFORMANCE WINGTIP DEVICE FOR
TRANSONIC AIRCRAFT |
|
| HENDARKO, H. |
ICAS 2002-5.3.3 |
DEVELOPMENT OF A HANDLING QUALITIES EVALUATION TOOLBOX ON THE BASIS OF
GIBSON CRITERIA |
|
| HENKNER, J. |
ICAS 2002-1.2.1 |
PRELIMINARY DESIGN PHASE 928JET - KEEPING THE 728JET FAMILY COMMONALITY |
|
| HENNE, P. |
ICAS 2002-8.7.5 |
TBD |
|
| HENZE, A. |
ICAS 2002-2.3.3 |
COMPUTATION INVESTIGATION IN REUSABLE SPACE TRANSPORT SYSTEMS AT SUPERSONIC
SPEED |
|
| HERBECK, L. |
ICAS 2002-3.4.1 (I.L.) |
DESIGN RULES FOR A CFRP OUTER WING |
|
| HEWITT, R.L. |
ICAS 2002-3.3.2 |
MODELING OF FULL-SCALE AIRCRAFT STRUCTURAL TESTS |
|
| HILLENHERMS, C. |
ICAS 2002-3.7.4 |
PITCH OSCILLATIONS OF A RECTANGULAR WING SECTION IN TRANSONIC FLOW |
|
| HIROSE, Y. |
ICAS 2002-3.4.3 |
THE CFRP SANDWICH PANEL FOR AIRCRAFT NOSE STRUCTURE |
|
| HITZEL, S.M. |
ICAS 2002-2.4.3 |
X-31A VECTOR HIGH ANGLE OF ATTACK DESCENT EULER AND NAVIER-STOKES SIMULATIONS
OF UNSTEADY MANOEUVRES |
|
| HO, C.M. |
ICAS 2002-5.5.1 (I.L.) |
FLIGHT DYNAMICS OF SMALL VEHICLES |
|
| HO, C-M. |
ICAS 2002-5.5.1 (I.L.) |
FLIGHT DYNAMICS OF SMALL VEHICLES |
|
| HOA, S.V. |
ICAS 2002-4.9.4 |
ANALYSIS IF TRIAX COMPOSITES FOR SATELLITE APPLICATIONS |
|
| HOEIJMAKERS, H.W.M. |
ICAS 2002-2.8.2 |
THREE-DIMENSIONAL CO-OPERATIVE INSTABILITIES IN WAKE VORTEX PAIRS |
|
| HOGAN, P. |
ICAS 2002-7.10.4 |
AN AUTOMATED SYSTEM FRAMEWORK FOR PRE-MISSION SUCCESS EVALUATION OF MEDICAL
EMERGENCY HELICOPTERS OPERATIONS - DEFINED MISSION CAPABILITY SUB-MODULE |
|
| HOLL, M. |
ICAS 2002-7.3.4 |
EXPERIMENTAL INVESTIGATION OF SIMULATED ICE ACCRETION ON TURBOPROP AIRCRAFT |
|
| HOLMBERG, G. |
ICAS 2002-6.5.2 |
A MODULAR APPROACH TO THE AIRCRAFT PRODUCT DEVELOPMENT CAPABILITY |
|
| HORST, P. |
ICAS 2002-1.4.3 |
WITH PUBLIC DOMAIN SOFTWARE TO INTEGRATED DESIGN AND ANALYSIS TOOLS |
|
| HOUDEVILLE, R. |
ICAS 2002-2.5.3 |
ADVANCED NUMERICAL SIMULATIONS ON STRUCTURED GRIDS FOR TRANSPORT AIRCRAFT,
USING AN EFFICIENT OBJECT ORIENTED SOLVER |
|
| HSIAO, F.B. |
ICAS 2002-R24 |
EXPERIMENTAL STUDY OF TURBULENT WAKE FLOW DEVELOPMENT BEHIND A FINITE
WING WITH HIGH ANGLE OF ATTACKS |
|
| HSIAO, F-B. |
ICAS 2002-R35 |
THE DEVELOPMENT OF A LOW COST AUTONOMOUS UAV SYSTEM |
|
| HSU, C-C. |
ICAS 2002-R24 |
EXPERIMENTAL STUDY OF TURBULENT WAKE FLOW DEVELOPMENT BEHIND A FINITE
WING WITH HIGH ANGLE OF ATTACKS |
|
| HU, T. C. J. |
ICAS 2002-5.8.1(IL) |
COMBUSTION TECHNOLOGY CHALLENGES FOR SMALL AVIATION GAS TURBINES |
|
| HU, Y. |
ICAS 2002-1.4.1 |
A NEW EFFECTIVE MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM |
|
| HUA, J. |
ICAS 2002-2.4.2 |
INVESTIGATION OF HIGH-LIFT, MILD-STALL WINGS |
|
| HUA, J. |
ICAS 2002-2.5.2 |
RECENT EXAMPLES ON DESIGN AERODYNAMICS FOR TRANSPORT AIRCRAFT |
|
| HUANG, W. |
ICAS 2002-2.1.4 |
A RAPID NUMERICAL METHOD FOR 3D AERO DYNAMICS DESIGN OF COMPRESSOR BLADE
ROW (APPLICATION TO A LOW SPEED EXPERIMENTAL MULTI-IDENTICAL-STAGE COMPRESSOR
DESIGN) |
|
| HUANG, X. |
ICAS 2002-3.9.2 |
ENHANCED MANEUVERABILITY BY ACTIVE VORTEX CONTROL WITH MOVEABLE BLOWING
JET |
|
| HUANG, X. |
ICAS 2002-R25 |
CENTRE-BODY AND LEADING-EDGE BEVEL EFFECTS ON DELTA WING AERODYNAMICS
AT HIGH INCIDENCE |
|
| HUI, K. |
ICAS 2002-7.8.3 |
KING AIR 350 FLIGHT-TEST DATA GATHERING AND LEVEL-D SIMULATOR AERODYNAMIC
MODEL DEVELOPMENT |
|
| HUNTER, C.A. |
ICAS 2002-2.10.2 |
SIMULATION OF FLOWS WITH PASSIVE POROSITY |
|
| HUZMEZAN, M. |
ICAS 2002-R26 |
RECONFIGURABLE CONTROL OF AN EXPERIMENTAL UNMANNED AIR VEHICLE (UAV) |
|
| HWANG, D.P. |
ICAS 2002-2.10.1 |
EXPERIMENTAL STUDY OF CHARACTERISTICS OF MICRO-HOLE POROUS SKINS FOR TURBULENT
SKIN FRICTION REDUCTION |
|
| HYDE, K. |
ICAS 2002-4.11.1 (I.L.) |
DISCOVERING THE SECRETS OF THE WRIGHT BROTHERS |
|
| IMUTA, M. |
ICAS 2002-3.4.3 |
THE CFRP SANDWICH PANEL FOR AIRCRAFT NOSE STRUCTURE |
|
| ISHIDE, T. |
ICAS 2002-3.11.3 |
CLARIFICATION OF UNSTEADY CHARACTERISTICS IN SEPARATED FLOW OVER AN AXISYMMETRIC
PARABOLOID AT HIGH ANGLES OF ATTACK |
|
| ISHMURATOV, F.Z. |
ICAS 2002-4.6.1 (I.L.) |
INVESTIGATIONS OF AIRSHIP AEROELASTICITY |
|
| ITO, K. |
ICAS 2002-8.1.4 |
OPTIMIZATION OF FLAPPING WING MOTION |
|
| ITOH, H. |
ICAS 2002-3.9.3 |
CONTROL OF CLOSED-TYPE SUPERSONIC CAVITY FLOWS |
|
| ITOH, S. |
ICAS 2002-7.1.2 |
RELIABILITY-BASED CALENDRIC INSPECTION SCHEDULE FOR AIRCRAFT STRUCTURES
WITH CORROSION FATIGUE |
|
| IUSO, G. |
ICAS 2002-2.10.4 |
DPIV INVESTIGATION OF A TURBULENT BOUNDARY LAYER MANIPULATED BY TRANSVERSAL
WALL OSCILLATIONS |
|
| IUSO, G. |
ICAS 2002-3.9.4 |
FLOW CONTROL DOWNSTREAM OF A BACKWARD FACING STEP: A DPIV STUDY |
|
| IVANTYSYNOVA, M. |
ICAS 2002-6.7.3 |
LOAD SIMULATOR BASED ON THE PRINCIPLE OF HYDROSTATIC SECONDARY CONTROL |
|
| JAHED-MOTLAGH, M.R. |
ICAS 2002-5.1.4 |
DESIGN OF MISSILE'S GUIDANCE SYSTEM BASED ON COMBINATION OF OPTIMAL PRESET
AND A TRANSCRIPTION OF FUNCTIONAL GUIDANCE |
|
| JAMBU, S. |
ICAS 2002-6.3.2 |
CREEP FORMING OF AlMgSc ALLOYS FOR AERONAUTIC AND SPACE APPLICATIONS |
|
| JAMESON, A. |
ICAS 2002-1.10.1 |
USING COMPUTATIONAL FLUID DYNAMICS FOR AERODYNAMICS - A CRITICAL ASSESSMENT |
|
| JAMONET, L. |
ICAS 2002-8.8.1 (St) |
THE CASE FOR A PRACTICAL SMALL SUPERSONIC TRANSPORT |
|
| JANICEK, L. |
ICAS 2002-R22 |
TECHNOLOGICAL TRENDS IN SIMULATION TECHNOLOGY IN AVIATION & PILOT TRAINIG |
|
| JARRY, P. |
ICAS 2002-0.5 |
MARKET DRIVERS AND INNNOVATION BEHIND THE AIRBUS PRODUCTS |
|
| JEANDEL, D. |
ICAS 2002-8.7.2 (I.L) |
A RESEARCH INITIATIVE ON THE SUPERSONIC AIRCRAFT |
|
| JENTINK, H.W. |
ICAS 2002-R28 |
A METHOD TO DERIVE THE USAGE OF HYDRAULIC ACTUATORS FROM FLIGHT DATA |
|
| JIANG, J. |
ICAS 2002-6.10.2 |
ACTIVE FAULT-TOLERANT CONTROL SYSTEM DESIGN FOR A TWO-ENGINE BLEED AIR
SYSTEM OF AN AIRCRAFT |
|
| JIAO, Z. |
ICAS 2002-6.7.3 |
LOAD SIMULATOR BASED ON THE PRINCIPLE OF HYDROSTATIC SECONDARY CONTROL |
|
| JIAO, Z. |
ICAS 2002-P7 |
REAL-TIME, DISTRIBUTED, PARALLEL SIMULATION OF HYDRAULIC SYSTEM BASED
ON LINUX IN THE NETWORK |
|
| JIAO, Z. |
ICAS 2002-R55 |
TORQUE CONTROL SYSTEM BASED ON COMPOUND CONTROL STRATEGIES FOR AERODYNAMIC
LOAD SIMULATOR |
|
| JODOIN, T.N.A. |
ICAS 2002-4.8.1 |
DIAGONAL TENSION IN FIBRE-METAL LAMINATES |
|
| JONES, D. |
ICAS 2002-2.4.5 |
INVERSE DESIGN OF HIGH LIFT SYSTEMS |
|
| JORGE, L.A.C. |
ICAS 2002-6.8.2 |
A MISSION PLANNER AND NAVIGATION SYSTEM FOR THE ARARA PROJECT |
|
| JOSLIN, R.D. |
ICAS 2002-8.4.1 (I.L.) |
FLOW AND NOISE CONTROL: TOWARD A CLOSER LINKAGE |
|
| JOUANNET, C. |
ICAS 2002-2.7.3 |
MODELING OF UNSTEADY AERODYNAMIC CHARACTERISTCS OF DELTA WINGS |
|
| JOUHAUD, J.-C. |
ICAS 2002-2.5.3 |
ADVANCED NUMERICAL SIMULATIONS ON STRUCTURED GRIDS FOR TRANSPORT AIRCRAFT,
USING AN EFFICIENT OBJECT ORIENTED SOLVER |
|
| JOZWIAK, R. |
ICAS 2002-P17 |
NEW TECHNOLOGY OF FLOW PATTERN CONTROL IN CASE OF AN AIRFOIL |
|
| JUHL, K. |
ICAS 2002-6.3.2 |
CREEP FORMING OF AlMgSc ALLOYS FOR AERONAUTIC AND SPACE APPLICATIONS |
|
| KAARLONEN, K. |
ICAS 2002-2.2.2 |
THE EFFECT OF THE REYNOLDS NUMBER ON THE WING VORTICES |
|
| KAFYEKE, F. |
ICAS 2002-3.10.1 |
DEVELOPMENT OF HIGH-LIFT SYSTEMS FOR THE BOMBARDIER CRJ-700 |
|
| KAINIKARA, S. |
ICAS 2002-7.10.3 |
A SYSTEM FRAMEWORK FOR THE DESIGN OF AIRCRAFT MISSION SYSTEMS FROM AN
OPERATOR'S PERSPECTIVE |
|
| KAINIKARA, S. |
ICAS 2002-R27 |
SYSTEM APPROACH TO IDENTIFY AEROSPACE RESEARCH CAPABILITIES AT UNIVERSITY |
|
| KALYGUINA, G.V. |
ICAS 2002-1.5.2 |
THE DOLPHIN: A NEW 100-SEAT AIRCRAFT IN LIFTING-FUSELAGE LAYOUT |
|
| KANNEMANS, H. |
ICAS 2002-R28 |
A METHOD TO DERIVE THE USAGE OF HYDRAULIC ACTUATORS FROM FLIGHT DATA |
|
| KARASHIMA, K. |
ICAS 2002-1.8.2 |
A STUDY ON REDUCTION OF AERODYNAMIC HEATING LOAD BY OPPOSING JET IN HYPERSONIC
FLOW |
|
| KARKLIN, S.G. |
ICAS 2002-1.5.2 |
THE DOLPHIN: A NEW 100-SEAT AIRCRAFT IN LIFTING-FUSELAGE LAYOUT |
|
| KARLSSON, M. |
ICAS 2002-5.3.2 |
AERODYNAMIC AND FLIGHT DYNAMIC REAL-TIME ANALYSIS DURING SPIN AND CAREFREE
MANEUVERING TESTS OF THE SAAB JAS39 GRIPEN |
|
| KAVSAOGLU, M.S. |
ICAS 2002-P6 |
MULTI BLOCK NAVIER STOKES SOLUTIONS OF LOW ASPECT RATIO RECTANGULAR FLAT
WINGS IN COMPRESSIBLE FLOW |
|
| KAVSAOGLU, M.S. |
ICAS 2002-R29 |
SOLUTION OF AIRFOIL-FLAP CONFIGURATIONS BY USING CHIMERA GRID SYSTEM |
|
| KAVSAOGLU, M.S. |
ICAS 2002-R30 |
MULTI BLOCK NAVIER STOKES SOLUTIONS OF LOW ASPECT RATIO RECTANGULAR FLAT
WINGS IN COMPRESSIBLE FLOW |
|
| KAWAKITA, T. |
ICAS 2002-5.1.2 |
3D-SIMULATION OF NONLINEAR DYNAMICS FOR A REENTRY VEHICLE |
|
| KAWALL, J.G. |
ICAS 2002-R68 |
INFLUENCE OF ACOUSTIC EXCITATION ON AIRFOIL PERFORMANCE AT LOW REYNOLDS
NUMBERS |
|
| KEARY, P. |
ICAS 2002-6.6.4 |
METHODOLOGY FOR ENSURING SAFETY OF AN EMBARKED HELICOPTER SECURING SYSTEM
PROBE INSTALLATION |
|
| KENNEDY, D. |
ICAS 2002-3.4.4 |
MULTILEVEL OPTIMIZATION OF AEROSPACE
AND LIGHTWEIGHT STRUCTURES |
|
| KERR, H.W. |
ICAS 2002-4.10.2 |
AN EVALUATION OF THE PHYSICAL PROPERTIES OF ND:YAG LASER WELDED HIGH
STRENGTH 6000 SERIES ALUMINUM ALLOYS |
|
| KHADIVI, T. |
ICAS 2002-2.10.5 |
FLOW CONTROL OVER THE WING OF A FIGHTER-TYPE CONFIGURATION USING BOUNDARY
LAYER SUCTION |
|
| KHADIVI, T. |
ICAS 2002-2.6.4 |
PARAMETRIC ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF LAUNCH VEHICLES
WITH STRAP-ON BOOSTERS |
|
| KHALID, M. |
ICAS 2002-1.1.3 |
EVALUATION OF THREE DECOMPOSITION MDO ALGORITHMS |
|
| KHALID, M. |
ICAS 2002-2.11.1 |
OPTIMIZATIONS OF AIRFOIL AND WING USING GENETIC ALGORITHM |
|
| KHALID, M. |
ICAS 2002-2.5.1 |
A CFD APPROACH TOWARDS MODELING BLADE/VORTEX IMPINGEMENT EFFECTS
AND BUFFETING OVER AIRFOILS |
|
| KHALID, M. |
ICAS 2002-3.7.5 |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE FLOWFIELD IN A BLOWDOWN
WIND TUNNEL |
|
| KHAN, A.A. |
ICAS 2002-1.3.4 |
DESIGNING AND DEVELOPMENT OF UNMANNED AERIAL VEHICLE |
|
| KHAN, S. |
ICAS 2002-R31 |
FLIGHT TRAJECTORIES OPTIMIZATION |
|
| KHAN, Z. M. |
ICAS 2002-4.9.3 |
DESIGN AND DEVELOPMENT OF OPTIC FIBER SMART STRUCTURES IN AEROSPACE VEHICLES |
|
| KHAN, ZAFAR |
ICAS 2002-R32 |
THE INFLUENCE OF MULTIPLE NESTED LAYER WAVINESS ON COMPRESSION STRENGTH
OF CARBON FIBER COMPOSITE MATERIALS |
|
| KHO, C. |
ICAS 2002-3.10.1 |
DEVELOPMENT OF HIGH-LIFT SYSTEMS FOR THE BOMBARDIER CRJ-700 |
|
| KHOT, N.S. |
ICAS 2002-4.4.5 |
INVESTIGATION OF SHOCK-INDUCED LCO OF A WING/STORE CONFIGURATIONUSING
THE TRANSONIC SMALL DISTURBANCE METHOD |
|
| KIKUKAWA, H. |
ICAS 2002-3.4.3 |
THE CFRP SANDWICH PANEL FOR AIRCRAFT NOSE STRUCTURE |
|
| KIM, C. |
ICAS 2002-R33 |
THE STUDY OF MONOTONICITY OF AUSM-TYPE SCHEMES IN SHOCK DISCONTINUITIES |
|
| KIM, C.J. |
ICAS 2002-7.4.2 |
FAST CALIBRATION TECHNIQUE FOR A GIMBALLED INERTIAL NAVIGATION SYSTEM |
|
| KIM, K.H. |
ICAS 2002-R33 |
THE STUDY OF MONOTONICITY OF AUSM-TYPE SCHEMES IN SHOCK DISCONTINUITIES |
|
| KIND, R.J. |
ICAS 2002-7.3.1 |
RECENT DEVELOPMENTS IN SCALING METHODS FOR ICING WIND TUNNEL TESTING AT
REDUCED SCALE |
|
| KING, R. |
ICAS 2002-3.9.4 |
FLOW CONTROL DOWNSTREAM OF A BACKWARD FACING STEP: A DPIV STUDY |
|
| KLEINAKIS, E. |
ICAS 2002-4.7.4 |
DIAGNOSTICS OF LEAKAGES IN GAS TURBINES |
|
| KNOLL, A. |
ICAS 2002-5.3.4 (I.L.) |
HIGH ANGLE OF ATTACK APPROACH AND LANDING CONTROL LAW DESIGN FOR THE X-31A |
|
| KNOLL, A. |
ICAS 2002-5.6.1 (I.L.) |
APPLICATION OF ESTOL FLIGHT CONTROL TECH-NOLOGY TO UCAV DESIGN |
|
| KNOWLES, K. |
ICAS 2002-3.6.2 |
NUMERICAL PREDICTIONS AND EXPERIMENTS ON SUPERSONIC JET MIXING FROM CASTELLATED
NOZZLES |
|
| KOBAYASHI, M.H. |
ICAS 2002-2.9.1 |
ON TRANSMISSION OF SOUND ACROSS A NON ISOTHERMAL BOUNDARY LAYER |
|
| KOCHERSBERGER, K. |
ICAS 2002-4.11.2 (I.L.) |
TEST AND EVALUATION OF THE WRIGHT BROTHERS AIRCRAFT, PROPELLERS AND ENGINES |
|
| KOENIG, R. |
ICAS 2002-4.6.4 |
IN-FLIGHT GUST AND LOAD MEASUREMENTS ON AN AIRSHIP FOR MODEL-BUILDING
AND COMPARISON WITH THE TRANSPORT AIRSHIP REQUIREMENTS |
|
| KOK, L. |
ICAS 2002-4.8.1 |
DIAGONAL TENSION IN FIBRE-METAL LAMINATES |
|
| KOK, L.J.J. |
ICAS 2002-3.4.2 |
OPTIMAL DESIGN OF FUSELAGE STRUCTURES |
|
| KONG, D. |
ICAS 2002-7.5.3 |
THE HIERARCHICAL AVAILABILITY ANALYSIS FOR FLIGHT CONTROL SYSTEM |
|
| KONG, F. |
ICAS 2002-2.4.2 |
INVESTIGATION OF HIGH-LIFT, MILD-STALL WINGS |
|
| KONG, F.M. |
ICAS 2002-2.5.2 |
RECENT EXAMPLES ON DESIGN AERODYNAMICS FOR TRANSPORT AIRCRAFT |
|
| KONYUKHOV, A.V. |
ICAS 2002-2.11.3 |
NUMERICAL SIMULATION OF FLOWS INTO INDUCTIVE
PLASMATRONS |
|
| KORDES, T. |
ICAS 2002-5.5.2 |
MODELING OF THE NONLINEAR DYNAMIC BEHAVIOR OF A MICRO-AERIAL-VEHICLE (MAV)
IN AN ENVIRONMENT OF A TURBULENT ATMOSPHERE |
|
| KOSTIC, I. |
ICAS 2002-R12 |
NUMERICAL MODEL OF SINGLE MAIN ROTOR HELICOPTER DYNAMICS |
|
| KOSTIC, I. |
ICAS 2002-R71 |
ADAPTIVE MODELING AND OPTIMIZATION OF PILOT HELMETS FOR DIFFERENT KINDS
OF IMPACTS WITH HARD OBSTACLES |
|
| KOSUGI, K. |
ICAS 2002-3.4.3 |
THE CFRP SANDWICH PANEL FOR AIRCRAFT NOSE STRUCTURE |
|
| KOSYKH, A.P. |
ICAS 2002-1.4.2 |
MULTIDISCIPLINARY OPTIMIZATION OF AIRCRAFT PARAMETERS BY THE LOCAL DISTRIBUTED
CRITERIA METHOD |
|
| KOTAPATI, R.B. |
ICAS 2002-R60 |
NUMERICAL INVESTIGATION ON THE FLOW CHARACTERISTICS OF A SUPERSONIC JET
IMPINGING ON AN AXI-SYMMETRIC DEFLECTOR |
|
| KOTSIOPOULOS, P. |
ICAS 2002-4.7.4 |
DIAGNOSTICS OF LEAKAGES IN GAS TURBINES |
|
| KOUL,, A.K. |
ICAS 2002-5.8.3 |
STRESS INTENSITY FACTOR CALCULATIONS FOR CRACKS EMANATING FROM BOLT HOLES
IN A JET ENGINE COMPRESSOR DISC |
|
| KREUZER, P. |
ICAS 2002-1.2.2 |
DEVELOPMENT AND INTEGRATION OF A NEW HIGH PERFORMANCE WINGTIP DEVICE FOR
TRANSONIC AIRCRAFT |
|
| KRIJNEN, J.A. |
ICAS 2002-7.11.3 |
ENVIRONMENTAL, ECONOMICAL AND TECHNICAL ASPECTS OF A CRYOPLANE IN THE
PRELIMINARY DESIGN PHASE |
|
| KROLIKOWSKI, G. |
ICAS 2002-6.6.2 |
DEVELOPING A NEW FLAP FOR A LIGHT UTILITY TRANSPORT AIRPLANE |
|
| KROLL, N. |
ICAS 2002-1.10.5 |
MEGAFLOW - A NUMERICAL FLOW SIMULATION TOOL FOR TRANSPORT AIRCRAFT DESIGN |
|
| KRUEGER, W. |
ICAS 2002-4.6.2 |
FLUID-STRUCTURE COUPLING USING CFD AND MULTIBODY SIMULATION METHODS |
|
| KRUS, K. |
ICAS 2002-8.3.2 |
CAPTIVE CARRY TESTING AS A MEANS FOR RAPID EVALUATION OF UAV HANDLING
QUALITIES |
|
| KRUS, P. |
ICAS 2002-2.7.3 |
MODELING OF UNSTEADY AERODYNAMIC CHARACTERISTCS OF DELTA WINGS |
|
| KUBRYNSKI, K. |
ICAS 2002-P17 |
NEW TECHNOLOGY OF FLOW PATTERN CONTROL IN CASE OF AN AIRFOIL |
|
| KUDO, K. |
ICAS 2002-5.9.2 |
CONCEPTUAL DESIGN OF AIRCRAFT ENGINE USING MULTIDISCIPLINARY DESIGN OPTIMIZATION
TECHNIQUE |
|
| KUDRYAVTSEV, V.A |
ICAS 2002-P1 |
AN-70 STOL AIRCRAFT CHARACTERISTICS AT HIGH ANGLES OF ATTACK AND TAKEOFF
AND LANDING CHARACTERISTICS |
|
| KULLBERG, E. |
ICAS 2002-7.9.3 |
A MODEL FOR SIMULATION OF FLIGHT PASSAGES THROUGH TRAILING TIP VORTICES |
|
| KUSHAN, M.C. |
ICAS 2002-8.6.3 |
EB VARESTRAINT TEST METHOD AND AN APPLICATION |
|
| KUSNI, M. |
ICAS 2002-8.5.2 |
THE ACTIVE NOISE CONTROL OF PROPELLER NOISE USING A MULTIPOLE SECONDARY
SOURCE |
|
| KUSUMO, R. |
ICAS 2002-1.3.2 |
A SYSTEM FRAMEWORK TO AUTOMATE DESIGN DECISION SUPPORT OF RE-CONFIGURABLE
UAVS |
|
| KUSUMO, R. |
ICAS 2002-6.1.3 |
COMMON DEVELOPMENT TOOLS FOR AN INTEGRATED DECISION SUPPORT SYSTEM FOR
MID-LIFE UPGRADE ANALYSIS |
|
| KUSUMO, R. |
ICAS 2002-7.10.3 |
A SYSTEM FRAMEWORK FOR THE DESIGN OF AIRCRAFT MISSION SYSTEMS FROM AN
OPERATOR'S PERSPECTIVE |
|
| KUSUMO, R. |
ICAS 2002-7.10.4 |
AN AUTOMATED SYSTEM FRAMEWORK FOR PRE-MISSION SUCCESS EVALUATION OF MEDICAL
EMERGENCY HELICOPTERS OPERATIONS - DEFINED MISSION CAPABILITY SUB-MODULE |
|
| KUSUMO, R. |
ICAS 2002-R73 |
A SYSTEM FRAMEWORK FOR THE DESIGN OF AN AVIONICS ARCHITECTURE WITH UPGRADE
POTENTIAL - AVIONICS ARCHITECTURE ANALYSIS MODULE |
|
| KUZMINA, S. |
ICAS 2002-4.3.2 |
REVIEW AND OUTLOOK ON ACTIVE AND PASSIVE AEROELASTIC DESIGN CONCEPTS FOR
FUTURE AIRCRAFT |
|
| KWAK, D.Y. |
ICAS 2002-8.7.3 |
LEADING-EDGE VORTEX FLAPS FOR SUPERSONIC TRANSPORT CONFIGURATION-EFFECTS
OF FLAP CONFIGURATIONS AND ROUNDED LEADING-EDGES |
|
| KYLE, H. |
ICAS 2002-3.11.2 |
DERIVATION OF UNSTEADY AERODYNAMIC MODELS FROM WIND TUNNEL MULTI-AXIS
TEST RIGS |
|
| LAINE, S. |
ICAS 2002-2.2.2 |
THE EFFECT OF THE REYNOLDS NUMBER ON THE WING VORTICES |
|
| LALIBERTE, J. |
ICAS 2002-R34 |
NUMERICAL MODELLING OF LOW-VELOCITY IMPACT DAMAGE IN FIBRE-METAL-LAMINATES |
|
| LAM, C.H. |
ICAS 2002-6.10.2 |
ACTIVE FAULT-TOLERANT CONTROL SYSTEM DESIGN FOR A TWO-ENGINE BLEED AIR
SYSTEM OF AN AIRCRAFT |
|
| LANDRY, N. |
|
THE CANADIAN AND AUSTRALIAN F/A-18 INTERNATIONAL FOLLOW-ON STRUCTURAL
TEST PROJECT |
|
| LANGLOIS, M. |
ICAS 2002-1.11.1 |
VALIDATION OF A NAVIER-STOKES SOLVER FOR AIRFOIL HIGH-LIFT ANALYSIS |
|
| LANGLOIS, R. |
ICAS 2002-6.6.4 |
METHODOLOGY FOR ENSURING SAFETY OF AN EMBARKED HELICOPTER SECURING SYSTEM
PROBE INSTALLATION |
|
| LANZI, L. |
ICAS 2002-4.9.1 |
EXPERIMENTAL BUCKLING TESTS AND NUMERICAL ANALYSES OF STIFFENED CYLINDRICAL
SHELLS IN COMPOSITE MATERIALS |
|
| LARSSON, R. |
ICAS 2002-7.9.3 |
A MODEL FOR SIMULATION OF FLIGHT PASSAGES THROUGH TRAILING TIP VORTICES |
|
| LARUELLE, G. |
ICAS 2002-6.4.3 (I.L.) |
AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN |
|
| LASCHKA, B. |
ICAS 2002-3.8.2 |
INVESTIGATIONS ON THE TURBULENT WAKE VORTEX FLOW OF LARGE TRANSPORT AIRCRAFT |
|
| LASEK, M. |
ICAS 2002-5.5.3 |
A STUDY OF FLIGHT DYNAMICS AND AUTOMATIC CONTROL OF AN ANIMALOPTER |
|
| LAWSON, N.J. |
ICAS 2002-1.6.3 |
SUPERSONIC BUSINESS JET AIRCRAFT DESIGN |
|
| LAWSON, N.J. |
ICAS 2002-3.6.2 |
NUMERICAL PREDICTIONS AND EXPERIMENTS ON SUPERSONIC JET MIXING FROM CASTELLATED
NOZZLES |
|
| LAWSON, W.H.S. |
ICAS 2002-4.10.2 |
AN EVALUATION OF THE PHYSICAL PROPERTIES OF ND:YAG LASER WELDED HIGH
STRENGTH 6000 SERIES ALUMINUM ALLOYS |
|
| LAYCOCK, K. |
ICAS 2002-7.10.4 |
AN AUTOMATED SYSTEM FRAMEWORK FOR PRE-MISSION SUCCESS EVALUATION OF MEDICAL
EMERGENCY HELICOPTERS OPERATIONS - DEFINED MISSION CAPABILITY SUB-MODULE |
|
| LE MOIGNE, Y. |
ICAS 2002-2.7.1 |
CFD SIMULATIONS OF THE UNSTEADY HIGH ALPHA AERODYNAMICS OF DELTA WINGS |
|
| LE PAPE, M.C. |
ICAS 2002-2.5.3 |
ADVANCED NUMERICAL SIMULATIONS ON STRUCTURED GRIDS FOR TRANSPORT AIRCRAFT,
USING AN EFFICIENT OBJECT ORIENTED SOLVER |
|
| LE POURHIET, A. |
ICAS 2002-3.9.5 |
MATHEMATICAL MODELLING AND ACTIVE CONTROL OF OSCILLATORS. APPLICATION
TO BUFFET AND TO COMPRESSOR SURGE. |
|
| LEBOURG, S. |
ICAS 2002-8.7.4 |
TECHNOLOGICAL AND DESIGN CHALLENGES FOR SUPERSONIC BUSINESS JET |
|
| LEBRUN, F. |
ICAS 2002-6.6.2 |
DEVELOPING A NEW FLAP FOR A LIGHT UTILITY TRANSPORT AIRPLANE |
|
| LEDERLE, S. |
ICAS 2002-8.8.1 (St) |
THE CASE FOR A PRACTICAL SMALL SUPERSONIC TRANSPORT |
|
| LEE, BEN H.K. |
ICAS 2002-4.2.2 |
LIMIT-CYCLE OSCILLATIONS OF AN AIRFOIL WITH PIECE-WISE LINEAR RESTORING
FORCES |
|
| LEE, K. |
ICAS 2002-R33 |
THE STUDY OF MONOTONICITY OF AUSM-TYPE SCHEMES IN SHOCK DISCONTINUITIES |
|
| LEE, M.T. |
ICAS 2002-R35 |
THE DEVELOPMENT OF A LOW COST AUTONOMOUS UAV SYSTEM |
|
| LEE, R. |
ICAS 2002-3.11.1 |
WIND TUNNEL TESTING TO DETERMINE UNSTEADY LOADS ON A HELICOPTER FUSELAGE
IN A SHIP AIRWAKE |
|
| LEE, T.M. |
ICAS 2002-R36 |
SIGNAL SUBSPACE IDENTIFICATION & NOISE REDUCTION OF FLIGHT TEST DATA WITH
TRUNCATED SINGULAR VALUE DECOMPOSITION |
|
| LEGA, M. |
ICAS 2002-4.10.5 |
DEVELOPMENT APPROACH AND TESTING OF AN UNMANNED AERIAL VEHICLE |
|
| LEHN-SCHIOLER, T. |
ICAS 2002-4.1.4 |
ON THE NONLINEAR DYNAMICS APPROACH OF MODELING THE BIFURCATION FOR TRANSONIC
LIMIT CYCLE FLUTTER |
|
| LEIGH, B.R. |
ICAS 2002-4.10.2 |
AN EVALUATION OF THE PHYSICAL PROPERTIES OF ND:YAG LASER WELDED HIGH
STRENGTH 6000 SERIES ALUMINUM ALLOYS |
|
| LEMOINE, M. |
ICAS 2002-7.7.2 |
AN OBJECT-ORIENTED METHODOLOGY FOR MANAGING THE COMPLEXITY OF ATM SYSTEMS |
|
| LENCZOWSKI, B. |
ICAS 2002-4.10.1 |
NEW LIGHTWEIGHT ALLOYS FOR WELDED AIRCRAFT STRUCTURES |
|
| LENCZOWSKI, B. |
ICAS 2002-6.3.2 |
CREEP FORMING OF AlMgSc ALLOYS FOR AERONAUTIC AND SPACE APPLICATIONS |
|
| LEVY, A. |
ICAS 2002-1.3.1 |
ADVANCED TECHNOLOGIES & APPROACHES FOR NEXT GENERATION UAVS |
|
| LI, F. |
ICAS 2002-R59 |
NUMERICAL SIMULATION OF THE STORE SEPARATION USING UNSTRUCTURED CARTESIAN
GRID |
|
| LI, K. |
ICAS 2002-P7 |
REAL-TIME, DISTRIBUTED, PARALLEL SIMULATION OF HYDRAULIC SYSTEM BASED
ON LINUX IN THE NETWORK |
|
| LI, W. |
ICAS 2002-1.4.1 |
A NEW EFFECTIVE MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM |
|
| LI, W. |
ICAS 2002-5.7.3 |
DETECTION AND ISOLATION OF CONTROL SURFACE EFFECTIVENESS LOSS IN AIRCRAFT
BY USING FILTER BANK APPROACH |
|
| LI, Y.I |
ICAS 2002-4.7.4 |
DIAGNOSTICS OF LEAKAGES IN GAS TURBINES |
|
| LI, Z. |
ICAS 2002-6.3.3 |
A UNIQUE SPRAY FORMING PROCESS FOR HIGH TEMPERATURE MATERIALS FOR AEROSPACE
APPLICATIONS |
|
| LI, Z. |
ICAS 2002-P8 |
THE VERFICATION OF FLIGHT TEST FOR AIORBORNE ELECTRO-OPTICAL DETECTING
SYSTEM |
|
| LI, Z. |
ICAS 2002-R11 |
BEND/TWIST COUPLING EFFECTS FOR UNSYMMETRICAL & UNBALANCED LAMINATE USED
IN AIRCRAFT WING STRUCTURE ANALYSIS |
|
| LIBRESCU, L. |
ICAS 2002-3.1.1 |
GEOMETRICALLY LINEAR/NONLINEAR SANDWICH STRUCTURES WITH ANISOTROPIC FACE
SHEETS: THEORY AND BEHAVIOR |
|
| LIBRESCU, L. |
ICAS 2002-4.3.1 |
EFFECTS OF PRETWIST AND PRESETTING ANGLES ON FREE VIBRATION OF ELASTICALLY
TAILORED ROTATING THIN-WALLED BEAMS |
|
| LIBRESCU, L. |
ICAS 2002-4.4.4 |
SUPERSONIC FLUTTER AND POST-FLUTTER CONTROL OF AN AIRCRAFT WING SECTION |
|
| LIEVEN, N.A.J. |
ICAS 2002-8.3.5 |
LASER VIBROMETRY BASED DETECTIONS OF DELAMINATIONS IN AEROSPACE COMPOSITES |
|
| LILLEY, G.M. |
ICAS 2002-8.11.4 (I.L.) |
CONCORDE’S LEGACY : CHANGES IN THE ENVIRONMENTAL SCENE. FROM 1976 TO TODAY |
|
| LIMBERG, W. |
ICAS 2002-3.7.4 |
PITCH OSCILLATIONS OF A RECTANGULAR WING SECTION IN TRANSONIC FLOW |
|
| LIN, K-W. |
ICAS 2002-R35 |
THE DEVELOPMENT OF A LOW COST AUTONOMOUS UAV SYSTEM |
|
| LIU, G. |
ICAS 2002-6.10.2 |
ACTIVE FAULT-TOLERANT CONTROL SYSTEM DESIGN FOR A TWO-ENGINE BLEED AIR
SYSTEM OF AN AIRCRAFT |
|
| LIU, H.H.T. |
ICAS 2002-R37 |
CONTROL INTEGRATION PROCESS IN AIRCRAFT SYSTEMS DEVELOPMENT |
|
| LIU, J.C. |
ICAS 2002-2.5.2 |
RECENT EXAMPLES ON DESIGN AERODYNAMICS FOR TRANSPORT AIRCRAFT |
|
| LIU, L. |
ICAS 2002-4.2.2 |
LIMIT-CYCLE OSCILLATIONS OF AN AIRFOIL WITH PIECE-WISE LINEAR RESTORING
FORCES |
|
| LIU, M. |
ICAS 2002-6.1.4 |
PROCESS MODELING AND REENGINEERING ON AIRCRAFT PRODUCT LIFECYCLE |
|
| LIU, Q. |
ICAS 2002-2.7.4 |
TRANSONIC AILERON BUZZ BOUNDARY PREDICTION USING HOPF-BIFURCATION ANALYSIS
METHOD |
|
| LIU, W-J. |
ICAS 2002-R24 |
EXPERIMENTAL STUDY OF TURBULENT WAKE FLOW DEVELOPMENT BEHIND A FINITE
WING WITH HIGH ANGLE OF ATTACKS |
|
| LIVERANI, A. |
ICAS 2002-6.8.3 |
SEMI-AUTOMATIC 3D FLIGHT SIMULATORSCENARIOS RECONSTRUCTION FROM GEOREFERENCED
AERIAL PHOTOS AND TERRESTRIAL MAPS |
|
| LLEWELLYN, E. |
ICAS 2002-8.3.2 |
CAPTIVE CARRY TESTING AS A MEANS FOR RAPID EVALUATION OF UAV HANDLING
QUALITIES |
|
| LOMBARDI, G. |
ICAS 2002-3.7.3 |
VALIDATION OF A WALL INTERFERENCE CORRECTION PROCEDURE |
|
| LOWENBERG, M.H. |
ICAS 2002-3.11.2 |
DERIVATION OF UNSTEADY AERODYNAMIC MODELS FROM WIND TUNNEL MULTI-AXIS
TEST RIGS |
|
| LOWENBERG, M.H. |
ICAS 2002-5.3.1 |
FEEDBACK STABILISED BIFURCATION TAILORING APPLIED TO AIRCRAFT MODELS |
|
| LU, G. |
ICAS 2002-P5 |
USING DATA MINING METHOD FOR ANALYZING OTS CAPTURE ZONE |
|
| LU, X. |
ICAS 2002-8.1.1 |
THE INVESTIGATION OF MULTI-DISCIPLINARY AND MULTI-OBJECTIVE OPTIMIZATION
METHOD FOR THE AIRCRAFT CONFIGURATION DESIGN |
|
| LUCKRING, J.M. |
ICAS 2002-2.4.1 |
AN OVERVIEW OF THE RTO SYMPOSIUM ON VORTEX FLOW AND HIGH ANGLE OF ATTACK
AERODYNAMICS |
|
| LUNGU, R. |
ICAS 2002-7.4.3 |
NON-LINEAR STRUCTURES FOR STABILISATION- AND PRECESSION AXIS COUPLING
OF THE ORIENTATION AND STABILISATION GYROSYSTEMS |
|
| LUSIGNAN, B. |
ICAS 2002-7.2.3 (I.L.) |
THE GLOBAL ROLE OF THE US-TOP UNIVERSITIES FOR THE PROVISION OF THE HUMAN
RESOURCES IN ENGINEERING SCIENCE TO THE AEROSPACE COMMUNITY |
|
| LUTZ, TH. |
ICAS 2002-P14 |
STRUCTURAL CONCEPTS AND AERODYNAMIC DESIGN OF SHOCK CONTROL BUMPS |
|
| LY, E. |
ICAS 2002-R39 |
TIME-LINEARISED TRANSONIC SMALL DISTURBANCE CODE INCLUDING ENTROPY AND
VORTICITY EFFECTS |
|
| LYE, J.D. |
ICAS 2002-3.10.3 |
TESTING OF A DASH 8 Q400 IN THE NASA AMES 80x120' WIND TUNNEL |
|
| LYSENKOV, A.M. |
ICAS 2002-1.5.2 |
THE DOLPHIN: A NEW 100-SEAT AIRCRAFT IN LIFTING-FUSELAGE LAYOUT |
|
| MAISON-LE POEC, S. |
ICAS 2002-4.9.2 |
INTEGRATED NUMERICAL ANALYSIS FOR COMPOSITE DAMAGE TOLERANCE |
|
| MALER, Z. |
ICAS 2002-7.1.3 |
SECURING OF THE SAFETY AND ECONOMY OF ACROBATIC AIRPLANE SERVICE |
|
| MALEV, H.U. |
ICAS 2002-7.6.4 |
RELATIONSHIP BETWEEN QUALITY ASSURANCE AND SAFETY |
|
| MALIK, R. |
ICAS 2002-7.6.4 |
RELATIONSHIP BETWEEN QUALITY ASSURANCE AND SAFETY |
|
| MAMOU, M. |
ICAS 2002-2.5.1 |
A CFD APPROACH TOWARDS MODELING BLADE/VORTEX IMPINGEMENT EFFECTS
AND BUFFETING OVER AIRFOILS |
|
| MARESCA, C. |
ICAS 2002-R6 |
CENTRIFUGAL AND 3D EFFECTS ON THE NEAR TIP SECTION OF ROTATING BLADE |
|
| MARIN, G. |
ICAS 2002-6.2.3 |
COST AND CYCLES REDUCTION BASED ON MANUFACTURING PROCESS SIMULATION |
|
| MARKISH, J. |
ICAS 2002-6.9.4 |
A VALUE-BASED APPROACH FOR COMMERCIAL AIRCRAFT CONCEPTUAL DESIGN |
|
| MARQUES, J.M.G. |
ICAS 2002-R71 |
ON WAKE VORTEX RESPONSE FOR SEVERAL COMBINATIONS
OF LEADING AND FOLLOWING AIRCRAFT |
|
| MARQUES, J.M.G. |
ICAS 2002-R8 |
ON THE CALCULATION OF COLLISION PROBABILITIES AS AN ASSURANCE OF SAFE
SEPARATION BETWEEN AIRCRAFT |
|
| MARSILIO, R. |
ICAS 2002-R40 |
IMPLEMENTATION AND VALIDATION OF THE SPALART-ALLMARAS TURBULENCE MODEL
FOR HIGH SPEED FLOWS |
|
| MARTENS, S. |
ICAS 2002-8.4.2 |
JET NOISE REDUCTION TECHNOLOGY DEVELOPMENT AT GE AIRCRAFT ENGINES |
|
| MARTIN, E. |
ICAS 2002-7.10.5 |
AN OPERATIONAL EVALUATION OF A TAKE-OFF PERFORMANCE MONITORING ALGORITHM |
|
| MARZOCCA, P. |
ICAS 2002-4.4.4 |
SUPERSONIC FLUTTER AND POST-FLUTTER CONTROL OF AN AIRCRAFT WING SECTION |
|
| MASSČ, B. |
ICAS 2002-5.9.1 |
NEW TECHNOLOGIES FOR EFFICIENT AND ENVIRONMENTALLY FRIENDLY AERO ENGINES |
|
| MATSUMURA, S. |
ICAS 2002-8.3.4 |
THERMODYNAMIC DESIGN OF AN ALTERNATIVE MONOPROPELLANT FOR EMERGENCY POWER
UNITS |
|
| MATSUNO, T. |
ICAS 2002-8.3.3 |
SMALL LEADING-EDGE FLAP FOR POST-STALL FLOW CONTROL ON A 45-DEG DELTA
WING |
|
| MATSUSHIMA, K. |
ICAS 2002-1.5.3 |
FLYING WING CONCEPT FOR MEDIUM SIZE AIRPLANE |
|
| MATSUSHITA, H. |
ICAS 2002-4.1.4 |
ON THE NONLINEAR DYNAMICS APPROACH OF MODELING THE BIFURCATION FOR TRANSONIC
LIMIT CYCLE FLUTTER |
|
| MATSUUCHI, K. |
ICAS 2002-2.10.3 |
ACTIVE SEPARATION CONTROL SYSTEM IMPROVED FOR CONTROL TIME AND SUPPRESSION
EFFECT |
|
| MAVRIPLIS, F. |
ICAS 2002-0.3 |
CFD IN CANADIAN AEROSPACE |
|
| MAVRIS, D. |
ICAS 2002-1.1.1 |
A PROBABILISTIC METHODOLOGY FOR THE TREATMENT OF SYSTEM-OF-SYSTEMS PROBLEMS
AND APPLICATION TO FUTURE AIR TRANSPORTATION ARCHITECTURES |
|
| MAVRIS, D.N. |
ICAS 2002-5.9.4 |
ADAPTIVE SELECTION OF PARETO OPTIMAL ENGINE TECHNOLOGY SOLUTION SETS |
|
| MCKINNEY, W.D. |
ICAS 2002-5.2.2 |
A LOW COST FLIGHT TEST INSTRUMENTATION PACKAGE FOR LIGHT AIRPLANES |
|
| MCKINNEY, W.D. |
ICAS 2002-6.6.2 |
DEVELOPING A NEW FLAP FOR A LIGHT UTILITY TRANSPORT AIRPLANE |
|
| MCMAHON, C.D. |
ICAS 2002-R61 |
INNOVATIVE TECHNIQUES FOR THE FINITE ELEMENT ANALYSIS AND OPTIMISATION
OF COMPOSITE STRUCTURES |
|
| MCMANUS, H. |
ICAS 2002-6.9.3 |
VALUE STREAM ANALYSIS AND MAPPING FOR PRODUCT DEVELOPMENT |
|
| MECHLER, H. |
ICAS 2002-R41 |
INTEGRATED PARAMETRIC AIRCRAFT DESIGN |
|
| MEIJER, J.J. |
ICAS 2002-4.3.4 |
TRANSONIC STATIC AEROELASTIC SIMULATIONS OF FIGHTER AIRCRAFT |
|
| MELO DE SOUSA, J.M. |
ICAS 2002-7.3.3 |
ON ICE BLOCKAGE OF VENT TUBES IN THE WING FUEL TANKS OF THE EPSILON AIRCRAFT |
|
| MEMON, I.R. |
ICAS 2002-R42 |
FATIGUE LIFE PREDICTION OF 3-D PROBLEMS BY DAMAGE MECHANICS WITH SPECTRUM
LOADING |
|
| MENDENHALL, M. |
ICAS 2002-2.3.4 |
LVX - AN INTEGRATED AERODYNAMIC DESIGN AND ANALYSIS METHOD |
|
| MERCURE, R.A. |
ICAS 2002-8.9.2 |
NASA’S SUPERSONIC COMMERCIAL AIRCRAFT TECHNOLOGY DEVELOPMENT – BACKGROUND
AND CURRENT STATUS |
|
| MEYER, O. |
ICAS 2002-3.7.2 |
EXPERIMENTAL INVESTIGATIONS ON THE ADAPTATION ACCURACY OF ADAPTIVE SLOTS
IN WIND TUNNEL TEST SECTION WALLS |
|
| MIAU, J.J. |
ICAS 2002-R43 |
NORMAL AND SIDE FORCES AMPLIFICATION BY LATERAL JET ISSUED FROM AN OGIVE
CYLINDER |
|
| MIKAMI, F. |
ICAS 2002-3.11.3 |
CLARIFICATION OF UNSTEADY CHARACTERISTICS IN SEPARATED FLOW OVER AN AXISYMMETRIC
PARABOLOID AT HIGH ANGLES OF ATTACK |
|
| MILLARD, R.L. |
ICAS 2002-6.9.3 |
VALUE STREAM ANALYSIS AND MAPPING FOR PRODUCT DEVELOPMENT |
|
| MILLET, C. |
ICAS 2002-2.9.2 |
RELATIONSHIP BETWEEN INSTABILITY WAVES AND NOISE OF LOW SUPERSONIC JETS |
|
| MIN, D. |
ICAS 2002-5.2.2 |
A LOW COST FLIGHT TEST INSTRUMENTATION PACKAGE FOR LIGHT AIRPLANES |
|
| MITROVIC, C. |
ICAS 2002-R12 |
NUMERICAL MODEL OF SINGLE MAIN ROTOR HELICOPTER DYNAMICS |
|
| MITROVIC, C. |
ICAS 2002-R71 |
ADAPTIVE MODELING AND OPTIMIZATION OF PILOT HELMETS FOR DIFFERENT KINDS
OF IMPACTS WITH HARD OBSTACLES |
|
| MIYAGAWA, HIROSHI |
ICAS 2002-5.9.2 |
CONCEPTUAL DESIGN OF AIRCRAFT ENGINE USING MULTIDISCIPLINARY DESIGN OPTIMIZATION
TECHNIQUE |
|
| MIYATA, K. |
ICAS 2002-8.7.3 |
LEADING-EDGE VORTEX FLAPS FOR SUPERSONIC TRANSPORT CONFIGURATION-EFFECTS
OF FLAP CONFIGURATIONS AND ROUNDED LEADING-EDGES |
|
| MIYATA, S. |
ICAS 2002-5.9.2 |
CONCEPTUAL DESIGN OF AIRCRAFT ENGINE USING MULTIDISCIPLINARY DESIGN OPTIMIZATION
TECHNIQUE |
|
| MIYATA, T. |
ICAS 2002-4.1.4 |
ON THE NONLINEAR DYNAMICS APPROACH OF MODELING THE BIFURCATION FOR TRANSONIC
LIMIT CYCLE FLUTTER |
|
| MOELYADI, M.A. |
ICAS 2002-R44 |
IMPROVEMENT OF TRANSONIC AEROFOIL AERODYNAMIC PERFORMANCE |
|
| MOENS, F. |
ICAS 2002-3.9.1 |
TRANSITION MEASUREMENT AND ANALYSIS ON A SWEPT WING IN HIGH LIFT CONFIGURATION |
|
| MOKHTARIAN, F. |
ICAS 2002-1.11.1 |
VALIDATION OF A NAVIER-STOKES SOLVER FOR AIRFOIL HIGH-LIFT ANALYSIS |
|
| MOLENT, L. |
ICAS 2002-0.6 |
THE CANADIAN AND AUSTRALIAN F/A-18 INTERNATIONAL FOLLOW-ON STRUCTURAL
TEST PROJECT |
|
| MONDOLONI, S. |
ICAS 2002-R45 |
TRAJECTORY MODELING ACCURACY FOR AIR TRAFFIC MANAGEMENT DECISION SUPPORT
TOOLS |
|
| MONDON, J-Y. |
ICAS 2002-6.5.1 (I.L.) |
THE EADS CORPORATE RESEARCH CENTER- NEW DIMENSIONS FOR THE FUTURE |
|
| MONK, J. |
ICAS 2002-5.10.4 |
THE AERODYNAMIC DESIGN OF AN OPTIMISED PROPELLER FOR A HIGH ALTITUDE LONG
ENDURANCE UAV |
|
| MOONEN, N.L.S. |
ICAS 2002-5.10.5 |
ENGINE INTAKE DOWNWASH FOR REAR FUSELAGE MOUNTED NACELLES |
|
| MOONEY, D.P. |
ICAS 2002-0.4 |
DEVELOPMENT AND APPLICATION OF TECHNOLOGY FOR THE SONIC CRUISER |
|
| MORA-CAMINO, F. |
ICAS 2002-5.7.2 |
NONLINEAR CONTROL LAW DESIGN FOR AUTO-FLARE |
|
| MORA-CAMINO, F. |
ICAS 2002-7.5.2 |
TRAJECTORY GENERATION AND DISPLAY FOR RELATIVE NAVIGATION OF TRANSPORTATION
AIRCRAFT |
|
| MORELLI, M. |
ICAS 2002-3.7.3 |
VALIDATION OF A WALL INTERFERENCE CORRECTION PROCEDURE |
|
| MORISHITA, E. |
ICAS 2002-3.9.3 |
CONTROL OF CLOSED-TYPE SUPERSONIC CAVITY FLOWS |
|
| MOSEKILDE, E. |
ICAS 2002-4.1.4 |
ON THE NONLINEAR DYNAMICS APPROACH OF MODELING THE BIFURCATION FOR TRANSONIC
LIMIT CYCLE FLUTTER |
|
| MOUSSA, Z.M. |
ICAS 2002-5.10.3 |
A STAGE CALCULATION IN A CENTRIFUGAL COMPRESSOR |
|
| MOUSTAPHA, H. |
ICAS 2002-4.7.5 |
EVOLUTION AND FUTURE TECHNOLOGY CHALLENGES FOR SMALL GAS TURBINES |
|
| MUELLER-WIESNER, D. |
ICAS 2002-6.5.1 (I.L.) |
THE EADS CORPORATE RESEARCH CENTER- NEW DIMENSIONS FOR THE FUTURE |
|
| MUHAMMAD, H. |
ICAS 2002-R22 |
AERODYNAMIC MODEL IDENTIFICATION OF THE N-250 AIRCRAFT BASED ON FLIGHT |
|
| MUNRO, C. |
ICAS 2002-8.3.2 |
CAPTIVE CARRY TESTING AS A MEANS FOR RAPID EVALUATION OF UAV HANDLING
QUALITIES |
|
| MURMAN, E. |
ICAS 2002-6.1.2 |
A FRAMEWORK FOR ACHIEVING LIFECYCLE VALUE IN AEROSPACE PRODUCT DEVELOPMENT |
|
| MURPHY, A. |
ICAS 2002-3.2.1 |
EFFICIENT NON-LINEAR MODELLING OF FUSELAGE PANELS |
|
| NAGABUSHAN, B. |
ICAS 2002-P9 |
DESIGN TRENDS AND GLOBAL DEVELOPMENTS IN MODERN LTA VEHICLES |
|
| NAGARAJAN, R. |
ICAS 2002-R78 |
HELICOPTER HYDRAULIC SYSTEM
(Design, Component Selection, Modular Construction,
Integration & Testing) |
|
| NAGHIB-LAHOUTI, A. |
ICAS 2002-2.6.4 |
PARAMETRIC ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF LAUNCH VEHICLES
WITH STRAP-ON BOOSTERS |
|
| NAKAHASHI, K. |
ICAS 2002-1.5.3 |
FLYING WING CONCEPT FOR MEDIUM SIZE AIRPLANE |
|
| NAKAMICHI, J. |
ICAS 2002-R39 |
TIME-LINEARISED TRANSONIC SMALL DISTURBANCE CODE INCLUDING ENTROPY AND
VORTICITY EFFECTS |
|
| NAKAMICHI, JIRO |
ICAS 2002-4.4.1 (I.L.) |
AILERON FLUTTER CALCULATION FOR A SUPERSONIC FUSELAGE-WING CONFIGURATION |
|
| NAKAMURA, Y. |
ICAS 2002-3.8.3 |
AERODYNAMIC CHARACTERISTICS OF SPIN PHENOMENON FOR DELTA WING |
|
| NAKAMURA, Y. |
ICAS 2002-8.3.3 |
SMALL LEADING-EDGE FLAP FOR POST-STALL FLOW CONTROL ON A 45-DEG DELTA
WING |
|
| NALBANTOGLU, V. |
ICAS 2002-R65 |
ACTIVE VIBRATION CONTROL OF A SMART PLATE |
|
| NANGIA, R.K. |
ICAS 2002-R46 |
ON DESIGN OF UNCONVENTIONAL HIGH ASPECT RATIO "JOINED-WING" TYPE AIRCRAFT |
|
| NARKIEWICZ, J. |
ICAS 2002-7.4.4 |
SIMULATION OF TERRAIN REFERENCE NAVIGATION SYSTEM BASED ON IMAGE MATCHING
FROM DIGITAL VIDEO CAMERA |
|
| NASSEF, H. |
ICAS 2002-5.5.1 (I.L.) |
FLIGHT DYNAMICS OF SMALL VEHICLES |
|
| NAUMAN, M. |
ICAS 2002-R23 |
SEPARATION CONTROL BY ALTERNATING TANGENTIAL BLOWING/SUCTION AT MULTIPLE
SLOTS |
|
| NEJAT, A. |
ICAS 2002-2.6.4 |
PARAMETRIC ANALYSIS OF AERODYNAMIC CHARACTERISTICS OF LAUNCH VEHICLES
WITH STRAP-ON BOOSTERS |
|
| NEMEC, M. |
ICAS 2002-1.7.3 |
FROM ANALYSIS TO DESIGN OF HIGH-LIFT CONFIGURATIONS USING A NEWTON-KRYLOV
ALGORITHM |
|
| NEMEC, M. |
ICAS 2002-6.6.2 |
DEVELOPING A NEW FLAP FOR A LIGHT UTILITY TRANSPORT AIRPLANE |
|
| NERIS, L.O. |
ICAS 2002-6.8.2 |
A MISSION PLANNER AND NAVIGATION SYSTEM FOR THE ARARA PROJECT |
|
| NERSESOV, G.G. |
ICAS 2002-1.4.2 |
MULTIDISCIPLINARY OPTIMIZATION OF AIRCRAFT PARAMETERS BY THE LOCAL DISTRIBUTED
CRITERIA METHOD |
|
| NESTERENKO, B.I. |
ICAS 2002-3.3.3* |
ANALYTICALLY-EXPERIMENTAL STUDY OF DAMAGE TOLERANCE OF AIRCRAFT STRUCTURES |
|
| NESTERENKO, G. |
ICAS 2002-3.3.1 |
SERVICE LIFE OF AIRPLANE STRUCTURES |
|
| NICKISON, D. |
ICAS 2002-3.10.3 |
TESTING OF A DASH 8 Q400 IN THE NASA AMES 80x120' WIND TUNNEL |
|
| NICOLOSI, F. |
ICAS 2002-5.2.1 |
FLYING QUALITIES ANALYSIS OF A THREE SURFACES AIRCRAFT MODEL |
|
| NIEWOEHNER, R. |
ICAS 2002-2.6.1 |
EVALUATION OF THE CAPABILITIES OF CFD TO PREDICT STORE TRAJECTORIES FROM
ATTACK AIRCRAFT |
|
| NIKUMB, S.K. |
ICAS 2002-R17 |
DESIGN OF SURFACE ROUGHNESS FOR PASSIVE FLOW CONTROL |
|
| NISHIKAWA, N. |
ICAS 2002-3.11.3 |
CLARIFICATION OF UNSTEADY CHARACTERISTICS IN SEPARATED FLOW OVER AN AXISYMMETRIC
PARABOLOID AT HIGH ANGLES OF ATTACK |
|
| NISHITANI, M. |
ICAS 2002-3.4.3 |
THE CFRP SANDWICH PANEL FOR AIRCRAFT NOSE STRUCTURE |
|
| NITSCHE, W. |
ICAS 2002-3.7.2 |
EXPERIMENTAL INVESTIGATIONS ON THE ADAPTATION ACCURACY OF ADAPTIVE SLOTS
IN WIND TUNNEL TEST SECTION WALLS |
|
| NITZSCHE, F. |
ICAS 2002-2.1.3 |
ROTORCRAFT AERODYNAMIC AND AEROACOUSTIC MODELLING USING VORTEX PARTICLE
METHODS |
|
| NITZSCHE, F. |
ICAS 2002-4.3.3 |
SMART SPRING CONCEPT FOR HELICOPTER VIBRATION AND NOISE CONTROL |
|
| NOGUCHI, M. |
ICAS 2002-2.8.1 |
EXPERIMENTAL AND NUMERICAL STUDY ON TRANSITION CHARACTERISTICS AT SUPERSONIC
SPEED |
|
| NOGUCHI, M. |
ICAS 2002-8.7.3 |
LEADING-EDGE VORTEX FLAPS FOR SUPERSONIC TRANSPORT CONFIGURATION-EFFECTS
OF FLAP CONFIGURATIONS AND ROUNDED LEADING-EDGES |
|
| NSI MBA, M. |
ICAS 2002-R6 |
CENTRIFUGAL AND 3D EFFECTS ON THE NEAR TIP SECTION OF ROTATING BLADE |
|
| OBAYASHI, S. |
ICAS 2002-4.4.1 (I.L.) |
AILERON FLUTTER CALCULATION FOR A SUPERSONIC FUSELAGE-WING CONFIGURATION |
|
| OCHI, A. |
ICAS 2002-1.7.2 |
A HYBRID UNSTRUCTURED GRID SYSTEM FOR VISCOUS AND INVISCID AERODYNAMIC
ANALYSIS |
|
| OH, S-Y. |
ICAS 2002-4.3.1 |
EFFECTS OF PRETWIST AND PRESETTING ANGLES ON FREE VIBRATION OF ELASTICALLY
TAILORED ROTATING THIN-WALLED BEAMS |
|
| OKTAY, E. |
ICAS 2002-R29 |
SOLUTION OF AIRFOIL-FLAP CONFIGURATIONS BY USING CHIMERA GRID SYSTEM |
|
| OKUNUKI, T. |
ICAS 2002-3.9.3 |
CONTROL OF CLOSED-TYPE SUPERSONIC CAVITY FLOWS |
|
| OLEJNIK, A. |
ICAS 2002-R19 |
EXTREME LOADS OF A TRAINER JET FOLLOWING A SUDDEN DEFLECTION OF CONTROL
SURFACE |
|
| OLESKIW, M.M. |
ICAS 2002-7.3.1 |
RECENT DEVELOPMENTS IN SCALING METHODS FOR ICING WIND TUNNEL TESTING AT
REDUCED SCALE |
|
| OLEVSKY, F. |
ICAS 2002-R9 |
MOTOR CASE FOR ROCKET TRAJECTORY CORRECTION SYSTEM |
|
| OLIVEIRA, J. M. G. S. |
ICAS 2002-8.4.4 |
ON THE ACOUSTIC MODES IN A CYLINDRICAL NOZZLE WITH AN ARBITRARY IMPEDANCE
DISTRIBUTION |
|
| ONORATO, M. |
ICAS 2002-2.10.4 |
DPIV INVESTIGATION OF A TURBULENT BOUNDARY LAYER MANIPULATED BY TRANSVERSAL
WALL OSCILLATIONS |
|
| ONORATO, M. |
ICAS 2002-3.9.4 |
FLOW CONTROL DOWNSTREAM OF A BACKWARD FACING STEP: A DPIV STUDY |
|
| ONYEBUEKE, L. |
ICAS 2002-7.6.1 |
EXPANDED ACCOMMODATION ANALYSIS AND RAPID PROTOTYPING
TECHNIQUE FOR THE DESIGN OF A CREW STATION COCKPIT |
|
| OPOKU, D.G. |
ICAS 2002-2.1.3 |
ROTORCRAFT AERODYNAMIC AND AEROACOUSTIC MODELLING USING VORTEX PARTICLE
METHODS |
|
| ORTIZ, R. |
ICAS 2002-7.1.1 |
ASSESMENT OF EXPLICIT F.E. CAPABILITIES FOR FULL SCALE COUPLED FLUID/STRUCTURE
AIRCRAFT DITCHING SIMULATIONS |
|
| OUATTARA, B |
ICAS 2002-7.5.2 |
TRAJECTORY GENERATION AND DISPLAY FOR RELATIVE NAVIGATION OF TRANSPORTATION
AIRCRAFT |
|
| OZELL, B. |
ICAS 2002-1.4.5 |
A CONFIGURABLE FRAMEWORK FOR MULTIDISCIPLINARY ANALYSIS INTEGRATION AND
MANAGEMENT |
|
| OZEM, H. |
ICAS 2002-5.8.1(IL) |
COMBUSTION TECHNOLOGY CHALLENGES FOR SMALL AVIATION GAS TURBINES |
|
| PAGLIONE, M. |
ICAS 2002-R45 |
TRAJECTORY MODELING ACCURACY FOR AIR TRAFFIC MANAGEMENT DECISION SUPPORT
TOOLS |
|
| PAGWIWOKO, C.P. |
ICAS 2002-R47 |
DYNAMIC MODELING AND TIME DOMAIN SIMULATION OF NON-LINEAR FLUTTER WITH
THE EXISTENCE OF FREE-PLAY MECHANISM |
|
| PALMER, M.E. |
ICAS 2002-R46 |
ON DESIGN OF UNCONVENTIONAL HIGH ASPECT RATIO "JOINED-WING" TYPE AIRCRAFT |
|
| PAMBAGJO, T.E. |
ICAS 2002-1.5.3 |
FLYING WING CONCEPT FOR MEDIUM SIZE AIRPLANE |
|
| PAPARONE, L. |
ICAS 2002-1.11.3 |
A METHOD FOR DRAG DECOMPOSITION FROM CFD CALCULATIONS |
|
| PARASCHIVOIU, M. |
ICAS 2002-R48 |
ILU PRECONDITIONED MULTI-MODEL FORMULATION FOR COMPRESSIBLE FLOWS ON 3D
UNSTRUCTURED MESHES |
|
| PARK, J.H. |
ICAS 2002-7.4.2 |
FAST CALIBRATION TECHNIQUE FOR A GIMBALLED INERTIAL NAVIGATION SYSTEM |
|
| PARVEZ, K. |
ICAS 2002-R23 |
SEPARATION CONTROL BY ALTERNATING TANGENTIAL BLOWING/SUCTION AT MULTIPLE
SLOTS |
|
| PASARIBU, H.M. |
ICAS 2002-R49 |
ANALYSIS OF FLIGHT PERFORMANCE AND STABILITY OF FAMILY OF TRANSPORT AIRPLANE
DESIGNS WITH FUSELAGE COMMONALITIES |
|
| PASCHEREIT, C.O. |
ICAS 2002-5.8.2 |
VORTEX BREAKDOWN CONTROL FOR REDUCED COMBUSTION PRESSURE PULSATIONS |
|
| PATEK, Z. |
ICAS 2002-7.3.4 |
EXPERIMENTAL INVESTIGATION OF SIMULATED ICE ACCRETION ON TURBOPROP AIRCRAFT |
|
| PEDDIE, C.L. |
ICAS 2002-8.11.3 (I.L.) |
NASA’S ULTRA EFFICIENT ENGINE TECHNOLOGY (UEET) PROGRAM – ENVIRONMENTAL
ELEMENTS |
|
| PELLEBERGS, J. |
ICAS 2002-7.5.1 |
AUTOMATIC AIRCRAFT COLLISION AVOIDANCE SYSTEM FOR AIR COMBAT MANEUVERING |
|
| PELLETIER, D. |
ICAS 2002-1.9.4 |
SENSITIVITY AND UNCERTAINTY ANALYSIS OF AERODYNAMIC FLOWS |
|
| PENN, D. |
ICAS 2002-1.3.1 |
ADVANCED TECHNOLOGIES & APPROACHES FOR NEXT GENERATION UAVS |
|
| PENTO, F. |
ICAS 2002-3.1.4 |
LOAD RESPONSE AND FAILURE OF THICK RTM COMPOSITE LUGS |
|
| PEPIN, F. |
ICAS 2002-3.10.1 |
DEVELOPMENT OF HIGH-LIFT SYSTEMS FOR THE BOMBARDIER CRJ-700 |
|
| PERNPEINTNER, A. |
ICAS 2002-7.2.1 (I.L.) |
THE WAY OF HARMONIZATION AND COOPERATION IN AEROSPACE EDUCATION IN EUROPE |
|
| PERRAUD, J. |
ICAS 2002-3.9.1 |
TRANSITION MEASUREMENT AND ANALYSIS ON A SWEPT WING IN HIGH LIFT CONFIGURATION |
|
| PERSIANI, F. |
ICAS 2002-6.8.3 |
SEMI-AUTOMATIC 3D FLIGHT SIMULATORSCENARIOS RECONSTRUCTION FROM GEOREFERENCED
AERIAL PHOTOS AND TERRESTRIAL MAPS |
|
| PERSSON, A. |
ICAS 2002-7.5.1 |
AUTOMATIC AIRCRAFT COLLISION AVOIDANCE SYSTEM FOR AIR COMBAT MANEUVERING |
|
| PETER, J. |
ICAS 2002-2.5.3 |
ADVANCED NUMERICAL SIMULATIONS ON STRUCTURED GRIDS FOR TRANSPORT AIRCRAFT,
USING AN EFFICIENT OBJECT ORIENTED SOLVER |
|
| PETILLON, O. |
ICAS 2002-4.10.3 |
NON DESTRUCTIVE INVESTIGATION TOOLS: VALUE CREATION FOR STRUCTURAL TEST
MONITORING |
|
| PFAENDER, H. |
ICAS 2002-1.1.1 |
A PROBABILISTIC METHODOLOGY FOR THE TREATMENT OF SYSTEM-OF-SYSTEMS PROBLEMS
AND APPLICATION TO FUTURE AIR TRANSPORTATION ARCHITECTURES |
|
| PICKARD, N. |
ICAS 2002-5.9.1 |
NEW TECHNOLOGIES FOR EFFICIENT AND ENVIRONMENTALLY FRIENDLY AERO ENGINES |
|
| PIETRUCHA, J. |
ICAS 2002-5.5.3 |
A STUDY OF FLIGHT DYNAMICS AND AUTOMATIC CONTROL OF AN ANIMALOPTER |
|
| PILIDIS, P. |
ICAS 2002-4.7.4 |
DIAGNOSTICS OF LEAKAGES IN GAS TURBINES |
|
| PIRACCINI, G. |
ICAS 2002-6.8.3 |
SEMI-AUTOMATIC 3D FLIGHT SIMULATORSCENARIOS RECONSTRUCTION FROM GEOREFERENCED
AERIAL PHOTOS AND TERRESTRIAL MAPS |
|
| PISTEK, A. |
ICAS 2002-R50 |
DEVELOPMENT OF A NEW GENERATION OF AIRCRAFT FOR PILOT TRAINING |
|
| PISTEK, A. |
ICAS 2002-R51 |
MATRIX FORMULATION OF WING LOADING DISTRIBUTION |
|
| PLOTKIN, K.J. |
ICAS 2002-8.11.2 |
SONIC BOOM PREDICTION AND MITIGATION |
|
| POGOSSYAN, |
ICAS 2002-R72 |
GENERATION OF SU-27 FIGHTER |
|
| POON, C. |
ICAS 2002-4.10.2 |
AN EVALUATION OF THE PHYSICAL PROPERTIES OF ND:YAG LASER WELDED HIGH
STRENGTH 6000 SERIES ALUMINUM ALLOYS |
|
| POON, C. |
ICAS 2002-4.8.1 |
DIAGONAL TENSION IN FIBRE-METAL LAMINATES |
|
| POON, C. |
ICAS 2002-R34 |
NUMERICAL MODELLING OF LOW-VELOCITY IMPACT DAMAGE IN FIBRE-METAL-LAMINATES |
|
| POON, C. |
ICAS 2002-R67 |
THIRTY YEARS OF RETROGRESSION AND REAGING |
|
| POPESCU, C.A. |
ICAS 2002-4.4.3 |
AN EXPERT DATA MINING SYSTEM FOR NONLINEAR AEROELASTIC RESPONSE PREDICTION |
|
| PORNSIN-SIRIRAK, N. |
ICAS 2002-5.5.1 (I.L.) |
FLIGHT DYNAMICS OF SMALL VEHICLES |
|
| PORRO, A.R. |
ICAS 2002-5.10.1 |
ON HAMMERSHOCK PROPAGATION IN A SUPERSONIC FLOW FIELD |
|
| PORTEMONT, G. |
ICAS 2002-7.1.1 |
ASSESMENT OF EXPLICIT F.E. CAPABILITIES FOR FULL SCALE COUPLED FLUID/STRUCTURE
AIRCRAFT DITCHING SIMULATIONS |
|
| POURADIER, J.M. |
ICAS 2002-7.8.1 (I.L.) |
HELICOPTER FLIGHT SAFETY ENHANCEMENT: A EUROCOPTER CONTINUING ACTION |
|
| PRANANTA, B.B. |
ICAS 2002-4.3.4 |
TRANSONIC STATIC AEROELASTIC SIMULATIONS OF FIGHTER AIRCRAFT |
|
| PRASAD, E. |
ICAS 2002-R65 |
ACTIVE VIBRATION CONTROL OF A SMART PLATE |
|
| PRICE, M. |
ICAS 2002-3.2.1 |
EFFICIENT NON-LINEAR MODELLING OF FUSELAGE PANELS |
|
| PRICE, M. |
ICAS 2002-R18 |
AN INVESTIGATION INTO THE EFFECTS OF EXPERIMENTAL ERRORS ON THE CORRELATION
BETWEEN FEA AND TEST RESULTS FOR A WELDED FUSELAGE PANEL |
|
| PRIJONO, E. |
ICAS 2002-2.11.2 |
COMPUTATIONAL STUDY OF THE AERODYNAMIC CHARACTERISTICS OF AXI-SYMMETRIC
BODIES IN TRANSONIC FLOW |
|
| PRITSCHOW, G. |
ICAS 2002-P14 |
STRUCTURAL CONCEPTS AND AERODYNAMIC DESIGN OF SHOCK CONTROL BUMPS |
|
| PRUDNIKOV, Y.A. |
ICAS 2002-3.10.5 |
ESTIMATION OF SPIN CHARACTERISTICS OF AEROBATIC AIRCRAFT BY MEANS OF SPIN
ROTATION MODELING IN HORIZONTAL WIND TUNNEL |
|
| PUSTOVOYTOV, V.P. |
ICAS 2002-P1 |
AN-70 STOL AIRCRAFT CHARACTERISTICS AT HIGH ANGLES OF ATTACK AND TAKEOFF
AND LANDING CHARACTERISTICS |
|
| QIAN, Y. |
ICAS 2002-R69 |
WAVERIDER DESIGN WITH PARAMETRIC FLOW QUALITY CONTROL BY INVERSE METHOD
OF CHARACTERISTICS |
|
| QIAO, Z. |
ICAS 2002-1.10.4 |
NUMERICAL OPTIMIZATION DESIGN OF WINGS BY SOLVING ADJOINT EQUATIONS |
|
| QIAO, Z. |
ICAS 2002-R53 |
NUMERICAL SIMULATION OF NAVIER-STOKES EQUATIONS FOR HELICOPTER ROTOR IN
FORWARD FLIGHT USING MOVING CHIMERA GRIDS |
|
| QIN, E. |
ICAS 2002-R59 |
NUMERICAL SIMULATION OF THE STORE SEPARATION USING UNSTRUCTURED CARTESIAN
GRID |
|
| QIU, D. |
ICAS 2002-2.5.2 |
RECENT EXAMPLES ON DESIGN AERODYNAMICS FOR TRANSPORT AIRCRAFT |
|
| QUEST, J. |
ICAS 2002-3.8.1 |
TESTING OF A MODERN TRANSPORT AIRCRAFT CONFIGURATION IN ETW CLOSE TO MACH
0.9 |
|
| QUIN, X.L. |
ICAS 2002-1.10.4 |
NUMERICAL OPTIMIZATION DESIGN OF WINGS BY SOLVING ADJOINT EQUATIONS |
|
| RADAKOVIC, D. |
ICAS 2002-R12 |
NUMERICAL MODEL OF SINGLE MAIN ROTOR HELICOPTER DYNAMICS |
|
| RAGHUNATHAN, S. |
ICAS 2002-2.8.3 |
PREDICTION OF LAMINAR-TO-TURBULENT TRANSITION IN INCOMPRESSIBLE FLOW PAST
3-D CAVITY |
|
| RAIZENNE, M.D. |
ICAS 2002-R67 |
THIRTY YEARS OF RETROGRESSION AND REAGING |
|
| RAJBHANDARI, S.P. |
ICAS 2002-8.6.2 |
AN APPROACH TO MODELLING AND PREDICTING IMPACT DAMAGE IN COMPOSITE STRUCTURES |
|
| RAJESWARA, R.M. |
ICAS 2002-R60 |
NUMERICAL INVESTIGATION ON THE FLOW CHARACTERISTICS OF A SUPERSONIC JET
IMPINGING ON AN AXI-SYMMETRIC DEFLECTOR |
|
| RALPH, J. |
ICAS 2002-5.1.1 |
THE EFFECT OF AIRCRAFT BIASES ON THE DELIVERY OF AN ENHANCED LASER-GUIDED
WEAPON |
|
| RALPH, J.F. |
ICAS 2002-5.7.1 |
MINIMISING THE RISK OF COLLATERAL DAMAGE WITH THE KALMAN-LEVY FILTER |
|
| RAND, O. |
ICAS 2002-3.2.3 |
ANALYTICAL APPROACH TO COMPOSITE BEAM ANALYSIS |
|
| RAO, N. |
ICAS 2002-R73 |
A SYSTEM FRAMEWORK FOR THE DESIGN OF AN AVIONICS ARCHITECTURE WITH UPGRADE
POTENTIAL - AVIONICS ARCHITECTURE ANALYSIS MODULE |
|
| RASUO, B. |
ICAS 2002-R54 |
AN EXPERIMENTAL METHODOLOGY FOR EVALUATING SURVIVABILITY OF AN AERONAUTICAL
CONSTRUCTIONS FROM COMPOSITE MATERIALS |
|
| RAUH, R. |
ICAS 2002-6.3.2 |
CREEP FORMING OF AlMgSc ALLOYS FOR AERONAUTIC AND SPACE APPLICATIONS |
|
| REBAINE, A. |
ICAS 2002-3.7.5 |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE FLOWFIELD IN A BLOWDOWN
WIND TUNNEL |
|
| RECKZEH, D. |
ICAS 2002-6.6.1 (I.L.)+C606 |
AERODYNAMIC DESIGN OF THE A380 HIGH-LIFT-WING |
|
| REHMET, M. |
ICAS 2002-6.9.2 |
CHALLENGES IN INTERNATIONAL CO-DESIGN AND DEVELOPMENT OF A NEW FAMILY
OF AIRLINERS |
|
| RENAUD, G. |
ICAS 2002-1.1.2 |
EVALUATION AND IMPLEMENTATION OF MULTIDISCIPLINARY DESIGN OPTIMIZATION
(MDO) STRATEGIES |
|
| RENAUD, G. |
ICAS 2002-R74 |
EVALUATION AND IMPLEMENTATION OF MULTIDISCIPLINARY DESIGN OPTIMIZATION
STRATEGIES |
|
| RHO, O. |
ICAS 2002-R33 |
THE STUDY OF MONOTONICITY OF AUSM-TYPE SCHEMES IN SHOCK DISCONTINUITIES |
|
| RIABOV, V.V. |
ICAS 2002-1.8.1 |
SIMULATION TECHNIQUES IN HYPERSONIC AEROTHERMODYNAMICS |
|
| RIABOV, V.V. |
ICAS 2002-P10 |
COMPUTATIONAL AND ANALYTICAL METHODS IN THE AIRCRAFT DESIGN CURRICULUM |
|
| RICCI, F. |
ICAS 2002-4.10.5 |
DEVELOPMENT APPROACH AND TESTING OF AN UNMANNED AERIAL VEHICLE |
|
| RICCIARDI, J. |
ICAS 2002-7.8.3 |
KING AIR 350 FLIGHT-TEST DATA GATHERING AND LEVEL-D SIMULATOR AERODYNAMIC
MODEL DEVELOPMENT |
|
| RICHTER, T. |
ICAS 2002-R41 |
INTEGRATED PARAMETRIC AIRCRAFT DESIGN |
|
| RIEGER, H. |
ICAS 2002-2.4.3 |
X-31A VECTOR HIGH ANGLE OF ATTACK DESCENT EULER AND NAVIER-STOKES SIMULATIONS
OF UNSTEADY MANOEUVRES |
|
| RINOIE, K. |
ICAS 2002-7.6.2 |
EFFICIENT EYE-SCANNING FOR REDUCING PILOT WORKLOAD-SINGLE PILOT IFR AND
VFR FLIGHT TESTS- |
|
| RINOIE, K. |
ICAS 2002-8.7.3 |
LEADING-EDGE VORTEX FLAPS FOR SUPERSONIC TRANSPORT CONFIGURATION-EFFECTS
OF FLAP CONFIGURATIONS AND ROUNDED LEADING-EDGES |
|
| RIZK, N. |
ICAS 2002-6.4.4 (I.L.) |
MODELING OF NOX FORMATION IN GAS TURBINE COMBUSTORS |
|
| RIZZI, A. |
ICAS 2002-2.7.1 |
CFD SIMULATIONS OF THE UNSTEADY HIGH ALPHA AERODYNAMICS OF DELTA WINGS |
|
| RODCHENKO, T.S. |
ICAS 2002-3.4.5 |
SERVICE LIFE OF A TITANIUM MAIN WING BOX FOR SECOND GENERATION SUPERSONIC
COMMERCIAL TRANSPORT |
|
| ROGERS, |
ICAS 2002-R55 |
PREDICTING CURE KINETICS FOR A NON-ISOTHERMAL CURE PROCESS WITH A CONVENTIONAL
ISOTHERMAL DSC TECHNIQUE. |
|
| ROHACS, J. |
ICAS 2002-7.11.2 |
EMISSION SCATTERING SIMULATION FOR AIR-PORT REGION |
|
| ROHACS, J. |
ICAS 2002-7.7.4 |
PATS PERSONAL AIR TRANSPORTATION SYSTEM |
|
| ROLSTON, S. |
ICAS 2002-3.8.1 |
TESTING OF A MODERN TRANSPORT AIRCRAFT CONFIGURATION IN ETW CLOSE TO MACH
0.9 |
|
| ROMANDER, E.A. |
ICAS 2002-2.1.2 |
COMPUTATIONAL SIMULATION OF PROPELLERS IN CRUISE |
|
| ROMEO, G. |
ICAS 2002-1.3.3 |
HELIPLAT: STRUCTURAL ANALYSIS OF HIGH ALTITUDE VERY-LONG ENDURANCE SOLAR
POWERED PLATFORM FOR TELECOMMUNICATION AND EARTH OBSERVATION APPLICATIONS |
|
| ROMEO, G. |
ICAS 2002-4.10.4 |
BEARING STRENGTH OF BOLTED JOINTS IN CFRP WING FITTINGS |
|
| ROSEN, M.A. |
ICAS 2002-R57 |
EXERGY BASED LOSS ANALYSIS OF A TURBOJET OVER A FLIGHT CYCLE |
|
| ROSSI, V. |
ICAS 2002-5.7.5 |
A FUZZY LOGIC AUTOPILOT DEVELOPMENT FOR A LIGHT TWIN ENGINE AIRCRAFT IN
THE APPROACH FLIGHT CONDITION |
|
| ROSSOW, C.C. |
ICAS 2002-1.10.5 |
MEGAFLOW - A NUMERICAL FLOW SIMULATION TOOL FOR TRANSPORT AIRCRAFT DESIGN |
|
| ROTH, B. |
ICAS 2002-5.9.4 |
ADAPTIVE SELECTION OF PARETO OPTIMAL ENGINE TECHNOLOGY SOLUTION SETS |
|
| ROUSSEL, J. |
|
THE CANADIAN AND AUSTRALIAN F/A-18 INTERNATIONAL FOLLOW-ON STRUCTURAL
TEST PROJECT |
|
| ROVENSKI, V. |
ICAS 2002-3.2.3 |
ANALYTICAL APPROACH TO COMPOSITE BEAM ANALYSIS |
|
| RUBIN, T. |
ICAS 2002-1.7.4 |
AN ACCURATE MULTIBLOCK ENO DRIVEN NAVIER-STOKES SOLVER FOR COMPLEX AERODYNAMIC
CONFIGURATIONS |
|
| RUBINSTEIN, R. |
ICAS 2002-1.7.5 |
STOCHASTIC MODELING OF LAMINAR-TURBULENT TRANSITION |
|
| RUDENKO, D.V. |
ICAS 2002-2.11.3 |
NUMERICAL SIMULATION OF FLOWS INTO INDUCTIVE
PLASMATRONS |
|
| RUSEK, J.J. |
ICAS 2002-8.3.4 |
THERMODYNAMIC DESIGN OF AN ALTERNATIVE MONOPROPELLANT FOR EMERGENCY POWER
UNITS |
|
| RYCKEBUSCH, C. |
ICAS 2002-2.6.1 |
EVALUATION OF THE CAPABILITIES OF CFD TO PREDICT STORE TRAJECTORIES FROM
ATTACK AIRCRAFT |
|
| RYZHOVA, T.B. |
ICAS 2002-R58 |
DEVELOPMENT OF ULTRASONIC METHOD OF RADIAL CLEARANCE ASSESSMENT FOR BOLTED
JOINTS AT RESTRICTED ACCESS |
|
| SAARELA, O. |
ICAS 2002-3.1.4 |
LOAD RESPONSE AND FAILURE OF THICK RTM COMPOSITE LUGS |
|
| SACHS, G. |
ICAS 2002-7.4.5 |
LOW-COST 3D-DISPLAY SYSTEM FOR LIGHT AIRCRAFT |
|
| SACHS, G. |
ICAS 2002-R75 |
SPEED CONTROL ISSUES OF 3D-TUNNEL/PREDICTOR DISPLAYS |
|
| SADDINGTON, A. |
ICAS 2002-3.6.2 |
NUMERICAL PREDICTIONS AND EXPERIMENTS ON SUPERSONIC JET MIXING FROM CASTELLATED
NOZZLES |
|
| SAGGIANI, G.M. |
ICAS 2002-5.7.5 |
A FUZZY LOGIC AUTOPILOT DEVELOPMENT FOR A LIGHT TWIN ENGINE AIRCRAFT IN
THE APPROACH FLIGHT CONDITION |
|
| SAKATA, K. |
ICAS 2002-1.6.1 (I.L.) |
SUPERSONIC EXPERIMENTAL AIRPLANE PROGRAM AND RELATED ACTIVITIES IN JAPAN |
|
| SALIKUDDIN, M. |
ICAS 2002-8.4.3 |
OPTIMIZATION OF ACOUSTIC LINER DESIGN FOR AXISYMMETRIC MIXER-EJECTOR NOZZLES
UNDER ESPR PROGRAM |
|
| SALMINEN, E. |
ICAS 2002-2.2.2 |
THE EFFECT OF THE REYNOLDS NUMBER ON THE WING VORTICES |
|
| SALTOGLU, R. |
ICAS 2002-6.8.4 |
ROBUST INTEGRATED INS/RADAR ALTIMETER ACCOUNTING FAULTS AT THE MEASUREMENT
CHANNELS |
|
| SALVETTI, M.V. |
ICAS 2002-3.7.3 |
VALIDATION OF A WALL INTERFERENCE CORRECTION PROCEDURE |
|
| SAMPATH, P. |
ICAS 2002-5.8.1(IL) |
COMBUSTION TECHNOLOGY CHALLENGES FOR SMALL AVIATION GAS TURBINES |
|
| SAMPATH, S. |
ICAS 2002-7.9.1 |
CAPACITY AND WAKE VORTICES |
|
| SANE, S.K. |
ICAS 2002-5.9.3 |
MODELING PROPULSION SYSTEM OF A SUBSONIC CIVIL JET AIRCRAFT FOR MULTIDISCIPLINARY
CONCEPTUAL DESIGN OPTIMIZATION |
|
| SANG, W. |
ICAS 2002-R59 |
NUMERICAL SIMULATION OF THE STORE SEPARATION USING UNSTRUCTURED CARTESIAN
GRID |
|
| SANGHI, V. |
ICAS 2002-5.9.3 |
MODELING PROPULSION SYSTEM OF A SUBSONIC CIVIL JET AIRCRAFT FOR MULTIDISCIPLINARY
CONCEPTUAL DESIGN OPTIMIZATION |
|
| SANKARAN, S. |
ICAS 2002-R60 |
NUMERICAL INVESTIGATION ON THE FLOW CHARACTERISTICS OF A SUPERSONIC JET
IMPINGING ON AN AXI-SYMMETRIC DEFLECTOR |
|
| SANTINI, P. |
ICAS 2002-7.2.2 (I.L.) |
THE CONTRIBUTION OF UNIVERSITY TO THE AEROSPACE RESEARCH AND TECHNOLOGIES |
|
| SANTOS, G.N. |
ICAS 2002-6.6.3 |
AERODYNAMIC ANALYSIS OF A BIPLANE AMPHIBIOUS LIGHT AIRCRAFT |
|
| SARA€YAKUPOGLU, T. |
ICAS 2002-8.6.3 |
EB VARESTRAINT TEST METHOD AND AN APPLICATION |
|
| SARAF, A. |
ICAS 2002-5.4.4 |
DESIGN OF STABILIZING AND LOCALLY-ROBUST NONLINEAR CONTROLLERS FOR A CLASS
OF NONLINEAR SYSTEMS |
|
| SARAVANAMUTTOO, H.I.H. |
ICAS2002-0.1 |
THE DANIEL AND FLORENCE GUGGENHEIM MEMORIAL LECTURE CIVIL PROPULSION;
THE LAST 50 YEARS |
|
| SASHIKUMA, H. |
ICAS 2002-3.4.3 |
THE CFRP SANDWICH PANEL FOR AIRCRAFT NOSE STRUCTURE |
|
| SATYANARAYANA, N. |
ICAS 2002-R60 |
NUMERICAL INVESTIGATION ON THE FLOW CHARACTERISTICS OF A SUPERSONIC JET
IMPINGING ON AN AXI-SYMMETRIC DEFLECTOR |
|
| SATYANARAYANA, T.N.V. |
ICAS 2002-R60 |
NUMERICAL INVESTIGATION ON THE FLOW CHARACTERISTICS OF A SUPERSONIC JET
IMPINGING ON AN AXI-SYMMETRIC DEFLECTOR |
|
| SCHERBAN, K.S. |
ICAS 2002-3.4.5 |
SERVICE LIFE OF A TITANIUM MAIN WING BOX FOR SECOND GENERATION SUPERSONIC
COMMERCIAL TRANSPORT |
|
| SCHETZ, J. |
ICAS 2002-4.7.1 |
NOVEL INJECTION SCHEME FOR JET INTERACTION FLOWS |
|
| SCHEUGENPFLUG, H. |
ICAS 2002-5.9.1 |
NEW TECHNOLOGIES FOR EFFICIENT AND ENVIRONMENTALLY FRIENDLY AERO ENGINES |
|
| SCHIECK, F. |
ICAS 2002-1.4.4 |
CONCEPTUAL DESIGN OPTIMISATION OF A "MALE" CONFIGURATION USING A FLEXIBLE
SCALING TOOL |
|
| SCHILLING, K. |
ICAS 2002-6.7.2 |
VIRTUAL LABORATORIES FOR SPACE ROBOTICS |
|
| SCHMIDT, N. |
ICAS 2002-0.6 |
THE CANADIAN AND AUSTRALIAN F/A-18 INTERNATIONAL FOLLOW-ON STRUCTURAL
TEST PROJECT |
|
| SCHMIDT, R.K. |
ICAS 2002-6.7.1 |
AN INTEGRATED MODULAR TEST RIG FOR LANDING GEAR FATIGUE AND STRENGTH TESTING |
|
| SCHMITT, D. |
ICAS 2002-1.5.1 |
DOES THE AIR TRANSPORT MARKET NEED "UN-CONVENTIONAL AIRCRAFT CONFIGURATIONS"? |
|
| SCHMITT, D. |
ICAS 2002-R41 |
INTEGRATED PARAMETRIC AIRCRAFT DESIGN |
|
| SCHNIEDER, H. |
ICAS 2002-7.7.3 |
A COST/BENEFIT ANALYSIS OF AFAS FUNCTIONALITIES FOR A FUTURE ATM-SYSTEM |
|
| SCHRAGE, D. |
ICAS 2002-1.1.1 |
A PROBABILISTIC METHODOLOGY FOR THE TREATMENT OF SYSTEM-OF-SYSTEMS PROBLEMS
AND APPLICATION TO FUTURE AIR TRANSPORTATION ARCHITECTURES |
|
| SCHROEDER, W. |
ICAS 2002-3.7.4 |
PITCH OSCILLATIONS OF A RECTANGULAR WING SECTION IN TRANSONIC FLOW |
|
| SCHULZ, H. |
ICAS 2002-7.10.1 |
DEVELOPMENT OF APPROACH PROCEDURE DESIGN CRITERIA FOR SYSTEMS BASED ON
GLOBAL NAVIGATION SATELLITE SYSTEM (GNSS) WITH GROUND BASED AUGMENTATION
SYSTEM (GBAS) |
|
| SCHWAMBORN, D. |
ICAS 2002-1.10.5 |
MEGAFLOW - A NUMERICAL FLOW SIMULATION TOOL FOR TRANSPORT AIRCRAFT DESIGN |
|
| SCHWEIGER, J. |
ICAS 2002-4.3.2 |
REVIEW AND OUTLOOK ON ACTIVE AND PASSIVE AEROELASTIC DESIGN CONCEPTS FOR
FUTURE AIRCRAFT |
|
| SCHYMANIETZ, K. |
ICAS 2002-6.5.1 (I.L.) |
THE EADS CORPORATE RESEARCH CENTER- NEW DIMENSIONS FOR THE FUTURE |
|
| SCHˇFER, D. |
ICAS 2002-7.7.3 |
A COST/BENEFIT ANALYSIS OF AFAS FUNCTIONALITIES FOR A FUTURE ATM-SYSTEM |
|
| SCOTT, M.L. |
ICAS 2002-3.1.3 |
A LINEAR 3-D FINITE ELEMENT UNIT CELL MODEL FOR FIBRE WAVINESS IN COMPOSITE
MATERIALS |
|
| SCOTT, M.L. |
ICAS 2002-6.10.1 |
MULTIDISCIPLINARY DESIGN OPTIMISATION FOR EMBEDDED SENSOR DESIGNS |
|
| SCOTT, M.L. |
ICAS 2002-8.6.2 |
AN APPROACH TO MODELLING AND PREDICTING IMPACT DAMAGE IN COMPOSITE STRUCTURES |
|
| SCOTT, M.L. |
ICAS 2002-R61 |
INNOVATIVE TECHNIQUES FOR THE FINITE ELEMENT ANALYSIS AND OPTIMISATION
OF COMPOSITE STRUCTURES |
|
| SCOTT, M.L. |
ICAS 2002-R62 |
CALCULATING THE COST OF A CARBON FIBRE COMPOSITE STRUCTURE FROM WITHIN
A FINITE ELEMENT MODEL |
|
| SEDIN, Y.C.J. |
ICAS 2002-7.9.3 |
A MODEL FOR SIMULATION OF FLIGHT PASSAGES THROUGH TRAILING TIP VORTICES |
|
| SEHRA, A. |
ICAS 2002-4.7.2 |
NASA'S FUTURE AEROPROPULSION VISION |
|
| SEMBENINI, G. |
ICAS 2002-8.2.2 |
HYPOTHESIS ON THE ENHANCING OF THE PROBABILITY OF SURVIVAL OF SPACE AND
TRANSATMOSPHERIC VEHICLES IN SPACE DEBRIS AND MICROMETEOROIDS CONTAMINATED
ENVIRONMENT |
|
| SEMBENINI, G.L. |
ICAS 2002-8.8.3 (St) |
ACCESSIBILITY AND MAINTAINABILITY STUDIES THROUGH DIGITAL HUMANS IN A
DIGITAL MOCK-UP CONTEXT |
|
| SEND, W. |
ICAS 2002-4.1.2 |
STABILITY ANALYSIS IN THE TIME-DOMAIN APPLIED TO ADAPTIVE TRANSPORT-AIRCRAFT
WINGS |
|
| SENNES, U. |
ICAS 2002-R75 |
SPEED CONTROL ISSUES OF 3D-TUNNEL/PREDICTOR DISPLAYS |
|
| SENSBURG, O. |
ICAS 2002-4.3.2 |
REVIEW AND OUTLOOK ON ACTIVE AND PASSIVE AEROELASTIC DESIGN CONCEPTS FOR
FUTURE AIRCRAFT |
|
| SERAUDIE, A. |
ICAS 2002-3.9.1 |
TRANSITION MEASUREMENT AND ANALYSIS ON A SWEPT WING IN HIGH LIFT CONFIGURATION |
|
| SEROR, S. |
ICAS 2002-1.7.4 |
AN ACCURATE MULTIBLOCK ENO DRIVEN NAVIER-STOKES SOLVER FOR COMPLEX AERODYNAMIC
CONFIGURATIONS |
|
| SHABTAI, M. |
ICAS 2002-R9 |
MOTOR CASE FOR ROCKET TRAJECTORY CORRECTION SYSTEM |
|
| SHAH, J. |
ICAS 2002-R18 |
AN INVESTIGATION INTO THE EFFECTS OF EXPERIMENTAL ERRORS ON THE CORRELATION
BETWEEN FEA AND TEST RESULTS FOR A WELDED FUSELAGE PANEL |
|
| SHANYGIN, A.N. |
ICAS 2002-1.4.2 |
MULTIDISCIPLINARY OPTIMIZATION OF AIRCRAFT PARAMETERS BY THE LOCAL DISTRIBUTED
CRITERIA METHOD |
|
| SHARMAN, D. |
ICAS 2002-8.8.1 (St) |
THE CASE FOR A PRACTICAL SMALL SUPERSONIC TRANSPORT |
|
| SHAW, R.S. |
ICAS 2002-6.4.1 (I.L.) |
ULTRA EFFICIENT ENGINE TECHNOLOGY PROGRAM |
|
| SHEN, G. |
ICAS 2002-7.4.1 (I.L.)+C672 |
A FAST AND PRECISION INITIAL ALIGNMENT METHOD FOR SINS ON STATIONARY BASE |
|
| SHEN, S. |
ICAS 2002-R80 |
APPLICATION OF FAULT DIAGNOSIS EXPERT SYSTEM FOR AIRCRAFT ELECTRIC POWER
SYSTEM |
|
| SHI, G. |
ICAS 2002-1.1.2 |
EVALUATION AND IMPLEMENTATION OF MULTIDISCIPLINARY DESIGN OPTIMIZATION
(MDO) STRATEGIES |
|
| SHI, G. |
ICAS 2002-4.8.1 |
DIAGONAL TENSION IN FIBRE-METAL LAMINATES |
|
| SHI, G. |
ICAS 2002-R74 |
EVALUATION AND IMPLEMENTATION OF MULTIDISCIPLINARY DESIGN OPTIMIZATION
STRATEGIES |
|
| SHIELDS, J.T. |
ICAS 2002-6.2.2 |
A HOLISTIC APPROACH TO MANUFACTURING SYSTEM DESIGN IN THE DEFENSE AEROSPACE
INDUSTRY |
|
| SHIMA, E. |
ICAS 2002-1.7.2 |
A HYBRID UNSTRUCTURED GRID SYSTEM FOR VISCOUS AND INVISCID AERODYNAMIC
ANALYSIS |
|
| SHIN, Y.J. |
ICAS 2002-7.4.2 |
FAST CALIBRATION TECHNIQUE FOR A GIMBALLED INERTIAL NAVIGATION SYSTEM |
|
| SIBILSKI, K. |
ICAS 2002-5.5.3 |
A STUDY OF FLIGHT DYNAMICS AND AUTOMATIC CONTROL OF AN ANIMALOPTER |
|
| SIERPUTOWSKI, P. |
ICAS 2002-P17 |
NEW TECHNOLOGY OF FLOW PATTERN CONTROL IN CASE OF AN AIRFOIL |
|
| SIIKONEN, T. |
ICAS 2002-2.2.2 |
THE EFFECT OF THE REYNOLDS NUMBER ON THE WING VORTICES |
|
| SILVA, W.A. |
ICAS 2002-4.4.4 |
SUPERSONIC FLUTTER AND POST-FLUTTER CONTROL OF AN AIRCRAFT WING SECTION |
|
| SIMONET, D. |
ICAS 2002-4.10.3 |
NON DESTRUCTIVE INVESTIGATION TOOLS: VALUE CREATION FOR STRUCTURAL TEST
MONITORING |
|
| SIMONOV, M.P. |
ICAS 2002-R72 |
GENERATION OF SU-27 FIGHTER |
|
| SIMPSON, D. L. |
ICAS 2002-0.6 |
THE CANADIAN AND AUSTRALIAN F/A-18 INTERNATIONAL FOLLOW-ON STRUCTURAL
TEST PROJECT |
|
| SIMS, S.W. |
ICAS 2002-5.7.1 |
MINIMISING THE RISK OF COLLATERAL DAMAGE WITH THE KALMAN-LEVY FILTER |
|
| SINGH, R. |
ICAS 2002-7.11.1 |
PROPULSION SYSTEM OPTIMISATION FOR MINIMUM GLOBAL WARMING POTENTIAL |
|
| SINHA, A.K. |
ICAS 2002-1.3.2 |
A SYSTEM FRAMEWORK TO AUTOMATE DESIGN DECISION SUPPORT OF RE-CONFIGURABLE
UAVS |
|
| SINHA, A.K. |
ICAS 2002-6.1.3 |
COMMON DEVELOPMENT TOOLS FOR AN INTEGRATED DECISION SUPPORT SYSTEM FOR
MID-LIFE UPGRADE ANALYSIS |
|
| SINHA, A.K. |
ICAS 2002-7.10.3 |
A SYSTEM FRAMEWORK FOR THE DESIGN OF AIRCRAFT MISSION SYSTEMS FROM AN
OPERATOR'S PERSPECTIVE |
|
| SINHA, A.K. |
ICAS 2002-7.10.4 |
AN AUTOMATED SYSTEM FRAMEWORK FOR PRE-MISSION SUCCESS EVALUATION OF MEDICAL
EMERGENCY HELICOPTERS OPERATIONS - DEFINED MISSION CAPABILITY SUB-MODULE |
|
| SINHA, A.K. |
ICAS 2002-R73 |
A SYSTEM FRAMEWORK FOR THE DESIGN OF AN AVIONICS ARCHITECTURE WITH UPGRADE
POTENTIAL - AVIONICS ARCHITECTURE ANALYSIS MODULE |
|
| SJOLANDER, S.A. |
ICAS 2002-5.11.4 |
IMPACT OF FLOW QUALITY IN TRANSONIC CASCADE WIND TUNNELS: MEASUREMENTS
IN AN HP TURBINE CASCADE |
|
| SJUNNESSON, G. |
ICAS 2002-1.6.4 |
GRIPEN FUTURE DEVELOPMENT |
|
| SLAMA, J. |
ICAS 2002-7.5.2 |
TRAJECTORY GENERATION AND DISPLAY FOR RELATIVE NAVIGATION OF TRANSPORTATION
AIRCRAFT |
|
| SLINGERLAND, R. |
ICAS 2002-5.10.5 |
ENGINE INTAKE DOWNWASH FOR REAR FUSELAGE MOUNTED NACELLES |
|
| SMITH, H. |
ICAS 2002-R16 |
DEVELOPMENT OF ENVIRONMENTALLY-FRIENDLY TECHNOLOGIES AND CONFIGURATIONS
FOR SUBSONIC JET TRANSPORTS |
|
| SMITH, W. |
ICAS 2002-6.4.5 (I.L.) |
T.B.D |
|
| SMYTH, R. |
ICAS 2002-6.10.4 |
SYSTEMS INTEGRATION – AIRBUS APPROACH |
|
| SNYDER, R.D. |
ICAS 2002-4.4.5 |
INVESTIGATION OF SHOCK-INDUCED LCO OF A WING/STORE CONFIGURATIONUSING
THE TRANSONIC SMALL DISTURBANCE METHOD |
|
| SOBIECZKY, H. |
ICAS 2002-R69 |
WAVERIDER DESIGN WITH PARAMETRIC FLOW QUALITY CONTROL BY INVERSE METHOD
OF CHARACTERISTICS |
|
| SOBRY, J.F. |
ICAS 2002-7.1.1 |
ASSESMENT OF EXPLICIT F.E. CAPABILITIES FOR FULL SCALE COUPLED FLUID/STRUCTURE
AIRCRAFT DITCHING SIMULATIONS |
|
| SOHI, N. |
ICAS 2002-3.10.5 |
ESTIMATION OF SPIN CHARACTERISTICS OF AEROBATIC AIRCRAFT BY MEANS OF SPIN
ROTATION MODELING IN HORIZONTAL WIND TUNNEL |
|
| SOLOMON, W. |
ICAS 2002-5.11.2 |
PERFORMANCE CHARACTERISTICS OF A REDUCED SOLIDITY LOW PRESSURE TURBINE |
|
| SOLTANI, M.R. |
ICAS 2002-2.10.5 |
FLOW CONTROL OVER THE WING OF A FIGHTER-TYPE CONFIGURATION USING BOUNDARY
LAYER SUCTION |
|
| SOMMERER, A. |
ICAS 2002-P14 |
STRUCTURAL CONCEPTS AND AERODYNAMIC DESIGN OF SHOCK CONTROL BUMPS |
|
| SONG, H. |
ICAS 2002-P11 |
AVIONICS DATA COMMUNICATION NETWORK MODELING AND ANALYSING |
|
| SONG, O. |
ICAS 2002-4.3.1 |
EFFECTS OF PRETWIST AND PRESETTING ANGLES ON FREE VIBRATION OF ELASTICALLY
TAILORED ROTATING THIN-WALLED BEAMS |
|
| SOUTIS, C. |
ICAS 2002-3.1.2 |
FAILURE PREDICTION OF STRINGER STIFFENED COMPOSITE PANELS WITH IMPACT
DAMAGE UNDER UNIAXIAL COMPRESSION |
|
| SPAZZINI, P.G. |
ICAS 2002-2.10.4 |
DPIV INVESTIGATION OF A TURBULENT BOUNDARY LAYER MANIPULATED BY TRANSVERSAL
WALL OSCILLATIONS |
|
| SPAZZINI, P.G. |
ICAS 2002-3.9.4 |
FLOW CONTROL DOWNSTREAM OF A BACKWARD FACING STEP: A DPIV STUDY |
|
| SPERL, R. |
ICAS 2002-7.4.5 |
LOW-COST 3D-DISPLAY SYSTEM FOR LIGHT AIRCRAFT |
|
| SPIECK, M. |
ICAS 2002-4.6.2 |
FLUID-STRUCTURE COUPLING USING CFD AND MULTIBODY SIMULATION METHODS |
|
| SRINIVASAN, R. |
ICAS 2002-7.8.3 |
KING AIR 350 FLIGHT-TEST DATA GATHERING AND LEVEL-D SIMULATOR AERODYNAMIC
MODEL DEVELOPMENT |
|
| SRIVASTAVA, B.N. |
ICAS 2002-5.10.3 |
A STAGE CALCULATION IN A CENTRIFUGAL COMPRESSOR |
|
| STAAF, M. |
ICAS 2002-5.3.2 |
AERODYNAMIC AND FLIGHT DYNAMIC REAL-TIME ANALYSIS DURING SPIN AND CAREFREE
MANEUVERING TESTS OF THE SAAB JAS39 GRIPEN |
|
| STANKE, A. |
ICAS 2002-6.1.2 |
A FRAMEWORK FOR ACHIEVING LIFECYCLE VALUE IN AEROSPACE PRODUCT DEVELOPMENT |
|
| STEENAERT, C.B. |
ICAS 2002-2.9.4 |
SIMPLIFIED DESIGN METHOD FOR A SYMMETRICAL WING-BODY FAIRING |
|
| STEIJL, R. |
ICAS 2002-2.8.2 |
THREE-DIMENSIONAL CO-OPERATIVE INSTABILITIES IN WAKE VORTEX PAIRS |
|
| STOICA, A. |
ICAS 2002-5.4.5 |
LATERAL FLIGHT CONTROL SYSTEM USING OPTIMAL H-INFINITY CONTROLLERS |
|
| STOTEN, D.P. |
ICAS 2002-5.3.1 |
FEEDBACK STABILISED BIFURCATION TAILORING APPLIED TO AIRCRAFT MODELS |
|
| STRAZNICKY, P.V. |
ICAS 2002-4.8.1 |
DIAGONAL TENSION IN FIBRE-METAL LAMINATES |
|
| STRAZNICKY, P.V. |
ICAS 2002-R34 |
NUMERICAL MODELLING OF LOW-VELOCITY IMPACT DAMAGE IN FIBRE-METAL-LAMINATES |
|
| STROEVE, S. |
ICAS 2002-7.9.2 |
SAFETY-SEPARATION ASSESSMENT OF SATELLITE-BASED EN-ROUTE ATC VERSUS CONVENTIONAL
EN-ROUTE ATC |
|
| STROEVE, S.H. |
ICAS 2002-R76 |
HUMAN COGNITION PERFORMANCE MODEL BASED EVALUATION OF SAFE SPACING IN
AIR TRAFFIC |
|
| STROHMAYER, A. |
ICAS 2002-1.5.1 |
DOES THE AIR TRANSPORT MARKET NEED "UN-CONVENTIONAL AIRCRAFT CONFIGURATIONS"? |
|
| SU, J. |
ICAS 2002-1.7.1 |
CALCULATION OF COMPRESSIBLE AND INCOMPRESSIBLE VISCOUS FLOWS BY A VISCOUS
INVISCID SPLITTING FINITE ELEMENT METHOD |
|
| SUGIMURA, Y. |
ICAS 2002-6.2.1 (I.L.)+C546 |
SOME MANUFACTURING ACTIVITIES IN JAPANESE AIRCRAFT INDUSTRIES (JAI) |
|
| SUGIURA, H. |
ICAS 2002-2.8.1 |
EXPERIMENTAL AND NUMERICAL STUDY ON TRANSITION CHARACTERISTICS AT SUPERSONIC
SPEED |
|
| SULLIVAN, P. |
ICAS 2002-R68 |
INFLUENCE OF ACOUSTIC EXCITATION ON AIRFOIL PERFORMANCE AT LOW REYNOLDS
NUMBERS |
|
| SUMITA, J. |
ICAS 2002-7.6.3 |
PROMOTING AUTONOMOUS CONTROL IN CIVIL TRANSPORTS AS A PROPOSAL FOR THE
FLIGHT COMMAND SYSTEM |
|
| SUN, L. |
ICAS 2002-P5 |
USING DATA MINING METHOD FOR ANALYZING OTS CAPTURE ZONE |
|
| SUN, Q. |
ICAS 2002-8.2.1 |
A SEMI-ANALYTICAL NUMERICAL METHOD OF DETERMINING STRESS INTENSITY FACTORS
FOR MULTIPLE SITES DAMAGE STRUCTURE |
|
| SUN, R.Z. |
ICAS 2002-2.5.2 |
RECENT EXAMPLES ON DESIGN AERODYNAMICS FOR TRANSPORT AIRCRAFT |
|
| SUNADA, Y. |
ICAS 2002-7.6.2 |
EFFICIENT EYE-SCANNING FOR REDUCING PILOT WORKLOAD-SINGLE PILOT IFR AND
VFR FLIGHT TESTS- |
|
| SUNDQVIST, B.G. |
ICAS 2002-7.5.1 |
AUTOMATIC AIRCRAFT COLLISION AVOIDANCE SYSTEM FOR AIR COMBAT MANEUVERING |
|
| SURACE, G. |
ICAS 2002-P12 |
EXPERIMENTAL ASSESSMENT AND ANALYSIS OF THE CREW WORKLOAD |
|
| SUTARTO, H.Y. |
ICAS 2002-R63 |
ROBUST FLUTTER MARGINS OF A TYPICAL WING SECTION USING WINDTUNNEL EXPERIMENT
DATA : A PRELIMINARY STUDY |
|
| SYMS, J. |
ICAS 2002-R64 |
VALIDATION OF ANALYTIC TOOL FOR SUBSCALE PROPELLER TESTS |
|
| SZABOLCSI, R. |
ICAS 2002-5.7.4 |
CONTROL LAW SYNTHESIS FOR AIRCRAFT AUTOPILOT WITH NONLINEAR ELEMENTS |
|
| T HART, W.G.J. |
ICAS 2002-8.6.1 |
PATCH REPAIR OF CRACKS IN THE UPPER LONGERON OF AN F-16 AIRCRAFT OF THE
ROYAL NETHERLANDS AIR FORCE (RNLAF) |
|
| TAHI, A. |
ICAS 2002-2.6.2 |
IAR STORES CLEARANCE CFD APPROACH:
FROM DEVELOPMENT TO AUTOMATED ENGINEERING TOOL |
|
| TAHIR, |
ICAS 2002-P13 |
COMPARISON OF 1D AND 2D NUMERICAL MODELS FOR PREDICTING HYPERSONIC INLET
FLOW STARTING |
|
| TAI, Y-C. |
ICAS 2002-5.5.1 (I.L.) |
FLIGHT DYNAMICS OF SMALL VEHICLES |
|
| TAKAGI, S. |
ICAS 2002-2.8.1 |
EXPERIMENTAL AND NUMERICAL STUDY ON TRANSITION CHARACTERISTICS AT SUPERSONIC
SPEED |
|
| TAKITA, K. |
ICAS 2002-5.11.1 |
RESEARCH ON APPLICATION OF CERAMIC TURBINE TO JET ENGINE |
|
| TAKOVITSKY, S. |
ICAS 2002-2.3.2 |
NUMERICAL OPTIMIZATION OF THE WING OF A SUPERSONIC AIRPLANE |
|
| TAPPI, M. |
ICAS 2002-6.8.3 |
SEMI-AUTOMATIC 3D FLIGHT SIMULATORSCENARIOS RECONSTRUCTION FROM GEOREFERENCED
AERIAL PHOTOS AND TERRESTRIAL MAPS |
|
| TARASOV, A.Z. |
ICAS 2002-R72 |
GENERATION OF SU-27 FIGHTER |
|
| TARHAN, E. |
ICAS 2002-R29 |
SOLUTION OF AIRFOIL-FLAP CONFIGURATIONS BY USING CHIMERA GRID SYSTEM |
|
| TEMLYAKOV, Y.N. |
ICAS 2002-3.10.5 |
ESTIMATION OF SPIN CHARACTERISTICS OF AEROBATIC AIRCRAFT BY MEANS OF SPIN
ROTATION MODELING IN HORIZONTAL WIND TUNNEL |
|
| THOMAS, J-M. |
ICAS 2002-6.5.1 (I.L.) |
THE EADS CORPORATE RESEARCH CENTER- NEW DIMENSIONS FOR THE FUTURE |
|
| THOMAS, R.H. |
ICAS 2002-8.4.1 (I.L.) |
FLOW AND NOISE CONTROL: TOWARD A CLOSER LINKAGE |
|
| THOMPSON, J. |
ICAS 2002-6.6.2 |
DEVELOPING A NEW FLAP FOR A LIGHT UTILITY TRANSPORT AIRPLANE |
|
| THOMPSON, R.S. |
ICAS 2002-8.6.2 |
AN APPROACH TO MODELLING AND PREDICTING IMPACT DAMAGE IN COMPOSITE STRUCTURES |
|
| THOMSON, R.S. |
ICAS 2002-3.1.3 |
A LINEAR 3-D FINITE ELEMENT UNIT CELL MODEL FOR FIBRE WAVINESS IN COMPOSITE
MATERIALS |
|
| THEVENET, P. |
ICAS 2002-4.9.2 |
INTEGRATED NUMERICAL ANALYSIS FOR COMPOSITE DAMAGE TOLERANCE |
|
| TI, W. |
ICAS 2002-R66 |
FLIGHT TEST MANAGEMENT AND COMMAND GUIDANCE SYSTEM FOR FLIGHT TEST |
|
| TIAN, S. |
ICAS 2002-6.3.3 |
A UNIQUE SPRAY FORMING PROCESS FOR HIGH TEMPERATURE MATERIALS FOR AEROSPACE
APPLICATIONS |
|
| TIKKA, J. |
ICAS 2002-3.3.4 |
FATIGUE LIFE EVALUATION OF CRITICAL LOCATIONS IN AIRCRAFT STRUCTURES USING
VIRTUAL FATIGUE TEST |
|
| TILMANN, C.P. |
ICAS 2002-R46 |
ON DESIGN OF UNCONVENTIONAL HIGH ASPECT RATIO "JOINED-WING" TYPE AIRCRAFT |
|
| TOGNACCINI, R. |
ICAS 2002-1.11.3 |
A METHOD FOR DRAG DECOMPOSITION FROM CFD CALCULATIONS |
|
| TOKUGAWA, N. |
ICAS 2002-2.8.1 |
EXPERIMENTAL AND NUMERICAL STUDY ON TRANSITION CHARACTERISTICS AT SUPERSONIC
SPEED |
|
| TOKUMASU, Y. |
ICAS 2002-6.4.2 (I.L.) |
PROGRAM OVERVIEW AND INTERMEDIATE ACHIEVEMENTS OF "RESEARCH AND DEVELOPMENT
OF ENVIRONMENTALLY COMPATIBLE PROPULSION SYSTEM FOR
NEXT-GENERATION SUPERSONIC TRANSPORT(ESPR PROJECT) |
|
| TREMEL, U. |
ICAS 2002-2.4.3 |
X-31A VECTOR HIGH ANGLE OF ATTACK DESCENT EULER AND NAVIER-STOKES SIMULATIONS
OF UNSTEADY MANOEUVRES |
|
| TREPANIER, J.Y. |
ICAS 2002-1.2.3 |
WING SHAPE OPTIMIZATION USING A CONSTRAINED NURBS SURFACE GEOMETRICAL
REPRESENTATION |
|
| TREPANIER, J.Y. |
ICAS 2002-1.4.5 |
A CONFIGURABLE FRAMEWORK FOR MULTIDISCIPLINARY ANALYSIS INTEGRATION AND
MANAGEMENT |
|
| TRIANTOS, D.G. |
ICAS 2002-2.1.3 |
ROTORCRAFT AERODYNAMIC AND AEROACOUSTIC MODELLING USING VORTEX PARTICLE
METHODS |
|
| TRINDADE, O. |
ICAS 2002-6.8.2 |
A MISSION PLANNER AND NAVIGATION SYSTEM FOR THE ARARA PROJECT |
|
| TSACH, S. |
ICAS 2002-1.3.1 |
ADVANCED TECHNOLOGIES & APPROACHES FOR NEXT GENERATION UAVS |
|
| TSAI, Y-F. |
ICAS 2002-R35 |
THE DEVELOPMENT OF A LOW COST AUTONOMOUS UAV SYSTEM |
|
| TSUKAMOTO, Y. |
ICAS 2002-5.11.1 |
RESEARCH ON APPLICATION OF CERAMIC TURBINE TO JET ENGINE |
|
| TUNG, C. |
ICAS 2002-7.9.1 |
CAPACITY AND WAKE VORTICES |
|
| TURCSANYI, O. |
ICAS 2002-7.6.4 |
RELATIONSHIP BETWEEN QUALITY ASSURANCE AND SAFETY |
|
| TURGEON, E. |
ICAS 2002-1.9.4 |
SENSITIVITY AND UNCERTAINTY ANALYSIS OF AERODYNAMIC FLOWS |
|
| UEDA, Y. |
ICAS 2002-2.8.1 |
EXPERIMENTAL AND NUMERICAL STUDY ON TRANSITION CHARACTERISTICS AT SUPERSONIC
SPEED |
|
| UTYUZHNIKOV, S.V. |
ICAS 2002-2.11.3 |
NUMERICAL SIMULATION OF FLOWS INTO INDUCTIVE
PLASMATRONS |
|
| VALERA, L.J. |
ICAS 2002-P9 |
DESIGN TRENDS AND GLOBAL DEVELOPMENTS IN MODERN LTA VEHICLES |
|
| VALLERANI, E. |
ICAS 2002-7.2.2 (I.L.) |
THE CONTRIBUTION OF UNIVERSITY TO THE AEROSPACE RESEARCH AND TECHNOLOGIES |
|
| VAN DER BURG, J.W. |
ICAS 2002-1.11.2 |
SHORT TURNAROUND TIME TURBULENT FLOW COMPUTATIONS FOR COMPLETE AIRCRAFT
CONFIGURATIONS |
|
| VAN DER PARK, M.N.J. |
ICAS 2002-7.9.2 |
SAFETY-SEPARATION ASSESSMENT OF SATELLITE-BASED EN-ROUTE ATC VERSUS CONVENTIONAL
EN-ROUTE ATC |
|
| VAN DER PARK, M.N.J. |
ICAS 2002-R76 |
HUMAN COGNITION PERFORMANCE MODEL BASED EVALUATION OF SAFE SPACING IN
AIR TRAFFIC |
|
| VAN DER WEIDE, E. |
ICAS 2002-2.4.3 |
X-31A VECTOR HIGH ANGLE OF ATTACK DESCENT EULER AND NAVIER-STOKES SIMULATIONS
OF UNSTEADY MANOEUVRES |
|
| VAN DER WEIDE, E.T.A. |
ICAS 2002-1.11.2 |
SHORT TURNAROUND TIME TURBULENT FLOW COMPUTATIONS FOR COMPLETE AIRCRAFT
CONFIGURATIONS |
|
| VAN OUDHEUSDEN, B.W. |
ICAS 2002-2.9.4 |
SIMPLIFIED DESIGN METHOD FOR A SYMMETRICAL WING-BODY FAIRING |
|
| VAN TOOR, J. |
ICAS 2002-1.4.4 |
CONCEPTUAL DESIGN OPTIMISATION OF A "MALE" CONFIGURATION USING A FLEXIBLE
SCALING TOOL |
|
| VANDERPOL, P. |
ICAS 2002-6.10.3 |
THE DESIGN AND DEVELOPMENT OF THE AIRBUS A380 MAIN LANDING GEARS |
|
| VASIL'EVSKII,, S.A. |
ICAS 2002-2.11.3 |
NUMERICAL SIMULATION OF FLOWS INTO INDUCTIVE
PLASMATRONS |
|
| VAUGHN, A. |
ICAS 2002-6.2.2 |
A HOLISTIC APPROACH TO MANUFACTURING SYSTEM DESIGN IN THE DEFENSE AEROSPACE
INDUSTRY |
|
| VILLERO, G. |
ICAS 2002-R77 |
PROPOSALS AND COMPARATIVE EVALUATION OF SYNTHETIC NONLINEAR MODELS IN
FLIGHT CONTROLS SIMULATION |
|
| VINET, A. |
ICAS 2002-4.9.2 |
INTEGRATED NUMERICAL ANALYSIS FOR COMPOSITE DAMAGE TOLERANCE |
|
| VIOLA, N. |
ICAS 2002-8.2.2 |
HYPOTHESIS ON THE ENHANCING OF THE PROBABILITY OF SURVIVAL OF SPACE AND
TRANSATMOSPHERIC VEHICLES IN SPACE DEBRIS AND MICROMETEOROIDS CONTAMINATED
ENVIRONMENT |
|
| VISVANATHAN, K. |
ICAS 2002-R60 |
NUMERICAL INVESTIGATION ON THE FLOW CHARACTERISTICS OF A SUPERSONIC JET
IMPINGING ON AN AXI-SYMMETRIC DEFLECTOR |
|
| VISWANATH, S. |
ICAS 2002-R78 |
HELICOPTER HYDRAULIC SYSTEM
(Design, Component Selection, Modular Construction,
Integration & Testing) |
|
| VITI, V. |
ICAS 2002-4.7.1 |
NOVEL INJECTION SCHEME FOR JET INTERACTION FLOWS |
|
| VOITCU, O. |
ICAS 2002-4.4.3 |
AN EXPERT DATA MINING SYSTEM FOR NONLINEAR AEROELASTIC RESPONSE PREDICTION |
|
| VOITYSHEN, V.S. |
ICAS 2002-1.4.2 |
MULTIDISCIPLINARY OPTIMIZATION OF AIRCRAFT PARAMETERS BY THE LOCAL DISTRIBUTED
CRITERIA METHOD |
|
| VON BOSE, H. |
ICAS 2002-0.2 |
AEROSPACE IN 2020 : EUROPEAN VISION |
|
| VOSS, R. |
ICAS 2002-4.1.2 |
STABILITY ANALYSIS IN THE TIME-DOMAIN APPLIED TO ADAPTIVE TRANSPORT-AIRCRAFT
WINGS |
|
| VOUTSINAS, S.G. |
ICAS 2002-2.1.3 |
ROTORCRAFT AERODYNAMIC AND AEROACOUSTIC MODELLING USING VORTEX PARTICLE
METHODS |
|
| V™RSMANN, P. |
ICAS 2002-5.5.2 |
MODELING OF THE NONLINEAR DYNAMIC BEHAVIOR OF A MICRO-AERIAL-VEHICLE (MAV)
IN AN ENVIRONMENT OF A TURBULENT ATMOSPHERE |
|
| WADEHN, W. |
ICAS 2002-P14 |
STRUCTURAL CONCEPTS AND AERODYNAMIC DESIGN OF SHOCK CONTROL BUMPS |
|
| WAECHTER, D. |
ICAS 2002-R65 |
ACTIVE VIBRATION CONTROL OF A SMART PLATE |
|
| WAGNER, S. |
ICAS 2002-P14 |
STRUCTURAL CONCEPTS AND AERODYNAMIC DESIGN OF SHOCK CONTROL BUMPS |
|
| WALLACE, W. |
ICAS 2002-R67 |
THIRTY YEARS OF RETROGRESSION AND REAGING |
|
| WALLER, G. |
ICAS 2002-2.7.5 |
CFD PREDICTION OF STABILITY DERIVATIVES OF A TURBOPROP AIRCRAFT USING
A CARTESIAN GRID BASED EULER CODE |
|
| WALLIN, M. |
ICAS 2002-3.1.4 |
LOAD RESPONSE AND FAILURE OF THICK RTM COMPOSITE LUGS |
|
| WALLIS, C. |
ICAS 2002-5.10.3 |
A STAGE CALCULATION IN A CENTRIFUGAL COMPRESSOR |
|
| WAN, T. |
ICAS 2002-2.2.1 |
NUMERICAL PREDICTION OF THE AIRFOIL ICE ACCRETION GROWTH |
|
| WANG, B. |
ICAS 2002-7.1.2 |
RELIABILITY-BASED CALENDRIC INSPECTION SCHEDULE FOR AIRCRAFT STRUCTURES
WITH CORROSION FATIGUE |
|
| WANG, J.J. |
ICAS 2002-2.5.2 |
RECENT EXAMPLES ON DESIGN AERODYNAMICS FOR TRANSPORT AIRCRAFT |
|
| WANG, S. |
ICAS 2002-7.5.3 |
THE HIERARCHICAL AVAILABILITY ANALYSIS FOR FLIGHT CONTROL SYSTEM |
|
| WANG, S. |
ICAS 2002-8.6.4 |
ACCELERATED LIFE TESTING FOR AERIAL MECHANICAL PRODUCTS |
|
| WANG, X. |
ICAS 2002-6.7.3 |
LOAD SIMULATOR BASED ON THE PRINCIPLE OF HYDROSTATIC SECONDARY CONTROL |
|
| WANG, X. |
ICAS 2002-7.4.1 (I.L.)+C672 |
A FAST AND PRECISION INITIAL ALIGNMENT METHOD FOR SINS ON STATIONARY BASE |
|
| WANG, X.F. |
ICAS 2002-5.3.1 |
FEEDBACK STABILISED BIFURCATION TAILORING APPLIED TO AIRCRAFT MODELS |
|
| WANG, Y. |
ICAS 2002-P15 |
A METHOD OF ESTIMATING AIRPLANE TURBULENCE USING WIND DATA |
|
| WERTENBERG, R. |
ICAS 2002-8.8.1 (St) |
THE CASE FOR A PRACTICAL SMALL SUPERSONIC TRANSPORT |
|
| WHELLENS, M. |
ICAS 2002-7.11.1 |
PROPULSION SYSTEM OPTIMISATION FOR MINIMUM GLOBAL WARMING POTENTIAL |
|
| WICKENS, R.H. |
ICAS 2002-4.11.3 (I.L.) |
PIONEERS OF FLIGHT IN CANADA |
|
| WICKRAMASINGHE, V.K. |
ICAS 2002-4.3.3 |
SMART SPRING CONCEPT FOR HELICOPTER VIBRATION AND NOISE CONTROL |
|
| WIJANARKO, B. |
ICAS 2002-R49 |
ANALYSIS OF FLIGHT PERFORMANCE AND STABILITY OF FAMILY OF TRANSPORT AIRPLANE
DESIGNS WITH FUSELAGE COMMONALITIES |
|
| WILFERT, G. |
ICAS 2002-5.9.1 |
NEW TECHNOLOGIES FOR EFFICIENT AND ENVIRONMENTALLY FRIENDLY AERO ENGINES |
|
| WILHITE, A. |
ICAS 2002-8.11.1 |
ENVIRONMENTAL ISSUES ADDDRESSED AND PROGRESS MADE UNDER THE HIGH SPEED
CIVIL TRANSPORT (HSCT) PROGRAM |
|
| WILLCOX, K. |
ICAS 2002-6.9.4 |
A VALUE-BASED APPROACH FOR COMMERCIAL AIRCRAFT CONCEPTUAL DESIGN |
|
| WILLSHIRE, W.L. |
ICAS 2002-8.5.1 (I.L.) |
NOISE REDUCTION TECHNOLOGY FOR THE 21ST CENTURY |
|
| WILMES, H. |
ICAS 2002-3.4.1 (I.L.) |
DESIGN RULES FOR A CFRP OUTER WING |
|
| WINKLER, E.R. |
ICAS 2002-7.6.1 |
EXPANDED ACCOMMODATION ANALYSIS AND RAPID PROTOTYPING
TECHNIQUE FOR THE DESIGN OF A CREW STATION COCKPIT |
|
| WITTENBERG, T.C. |
ICAS 2002-4.8.2 |
PLASTICITY CORRECTION FACTORS FOR BUCKLING OF FLAT RECTANGULAR GLARE PLATES
LOADED IN COMPRESSION OR SHEAR |
|
| WLEZIEN, R. |
ICAS 2002-8.9.1 |
DARPA’S QUIET SUPERSONIC PLATFORM (QSP) PROGRAM |
|
| WOLF, H.C.J. |
ICAS 2002-6.9.2 |
CHALLENGES IN INTERNATIONAL CO-DESIGN AND DEVELOPMENT OF A NEW FAMILY
OF AIRLINERS |
|
| WONG, P.W.C. |
ICAS 2002-3.7.1 |
HIGH REYNOLDS NUMBER SIMULATION IN A TRANSONIC WIND TUNNEL BY SURFACE
SUCTION |
|
| WONG, Y.S. |
ICAS 2002-4.2.2 |
LIMIT-CYCLE OSCILLATIONS OF AN AIRFOIL WITH PIECE-WISE LINEAR RESTORING
FORCES |
|
| WONG, Y.S. |
ICAS 2002-4.4.3 |
AN EXPERT DATA MINING SYSTEM FOR NONLINEAR AEROELASTIC RESPONSE PREDICTION |
|
| WOOD, R.M. |
ICAS 2002-8.7.1 (I.L.) |
AERODYNAMIC DESIGN OPPORTUNITIES FOR FUTURE SUPERSONIC AIRCRAFT |
|
| WRIGHT, C. |
ICAS 2002-8.2.3 |
EXPERIMENTAL STUDY OF THE STRUCTURE AND DEVELOPMENT OF A WINGTIP VORTEX
IN THE NEAR-FIELD |
|
| WRIGHT, M.C.N. |
ICAS 2002-3.8.1 |
TESTING OF A MODERN TRANSPORT AIRCRAFT CONFIGURATION IN ETW CLOSE TO MACH
0.9 |
|
| WU, C-R. |
ICAS 2002-R35 |
THE DEVELOPMENT OF A LOW COST AUTONOMOUS UAV SYSTEM |
|
| WU, L. |
ICAS 2002-8.2.1 |
A SEMI-ANALYTICAL NUMERICAL METHOD OF DETERMINING STRESS INTENSITY FACTORS
FOR MULTIPLE SITES DAMAGE STRUCTURE |
|
| WU, X. |
ICAS 2002-R67 |
THIRTY YEARS OF RETROGRESSION AND REAGING |
|
| WU, X.J. |
ICAS 2002-4.8.3 |
A HIGHER-ORDER THEORY FOR FIBER-METAL LAMINATES |
|
| WULFF, G. |
ICAS 2002-4.6.4 |
IN-FLIGHT GUST AND LOAD MEASUREMENTS ON AN AIRSHIP FOR MODEL-BUILDING
AND COMPARISON WITH THE TRANSPORT AIRSHIP REQUIREMENTS |
|
| XIANG, J.W. |
ICAS 2002-2.4.2 |
INVESTIGATION OF HIGH-LIFT, MILD-STALL WINGS |
|
| XIU, Y. |
ICAS 2002-R11 |
BEND/TWIST COUPLING EFFECTS FOR UNSYMMETRICAL & UNBALANCED LAMINATE USED
IN AIRCRAFT WING STRUCTURE ANALYSIS |
|
| XU, T. |
ICAS 2002-R48 |
ILU PRECONDITIONED MULTI-MODEL FORMULATION FOR COMPRESSIBLE FLOWS ON 3D
UNSTRUCTURED MESHES |
|
| XU, Y. |
ICAS 2002-2.1.4 |
A RAPID NUMERICAL METHOD FOR 3D AERO DYNAMICS DESIGN OF COMPRESSOR BLADE
ROW (APPLICATION TO A LOW SPEED EXPERIMENTAL MULTI-IDENTICAL-STAGE COMPRESSOR
DESIGN) |
|
| YAMADA, T. |
ICAS 2002-3.8.3 |
AERODYNAMIC CHARACTERISTICS OF SPIN PHENOMENON FOR DELTA WING |
|
| YAMAN, Y. |
ICAS 2002-R65 |
ACTIVE VIBRATION CONTROL OF A SMART PLATE |
|
| YAN, C. |
ICAS 2002-P16 |
REDUCED THRUST TAKEOFF |
|
| YAN, M. |
ICAS 2002-6.3.3 |
A UNIQUE SPRAY FORMING PROCESS FOR HIGH TEMPERATURE MATERIALS FOR AEROSPACE
APPLICATIONS |
|
| YANG, A.M. |
ICAS 2002-R53 |
NUMERICAL SIMULATION OF NAVIER-STOKES EQUATIONS FOR HELICOPTER ROTOR IN
FORWARD FLIGHT USING MOVING CHIMERA GRIDS |
|
| YANG, C-C. |
ICAS 2002-R35 |
THE DEVELOPMENT OF A LOW COST AUTONOMOUS UAV SYSTEM |
|
| YANG, G. |
ICAS 2002-4.4.1 (I.L.) |
AILERON FLUTTER CALCULATION FOR A SUPERSONIC FUSELAGE-WING CONFIGURATION |
|
| YANG, X.D. |
ICAS 2002-1.10.4 |
NUMERICAL OPTIMIZATION DESIGN OF WINGS BY SOLVING ADJOINT EQUATIONS |
|
| YARAS, M. |
ICAS 2002-1.9.2 |
AN EVALUATION OF SEVERAL LOW-RE TURBULENCE MODELS PART 1- FLAT-PLATE BOUNDARY
LAYER AND AXISYMMETRIC SEPARATING FLOWS |
|
| YARUSEVYCH, S. |
ICAS 2002-R68 |
INFLUENCE OF ACOUSTIC EXCITATION ON AIRFOIL PERFORMANCE AT LOW REYNOLDS
NUMBERS |
|
| YAZDANIAN, K. |
ICAS 2002-7.10.2 |
RELATIONAL MODEL AND DATA LINK FOR AIRCRAFT CONTROL DURING LANDING AND
TAKE-OFF |
|
| YIN, J. |
ICAS 2002-R79 |
INFLUENCE OF INLET PROFILE ON HIGH-BPR
TURBOFAN PERFORMANCE USING A RADIAL
PROFILE MAP |
|
| YOKOUCHI, S. |
ICAS 2002-8.3.3 |
SMALL LEADING-EDGE FLAP FOR POST-STALL FLOW CONTROL ON A 45-DEG DELTA
WING |
|
| YOKOYAMA, N. |
ICAS 2002-5.1.3 |
TRAJECTORY OPTIMIZATION OF SPACE PLANE USING GENETIC ALGORITHM COMBINED
WITH GRADIENT METHOD |
|
| YONG, D.G. |
ICAS 2002-4.3.3 |
SMART SPRING CONCEPT FOR HELICOPTER VIBRATION AND NOISE CONTROL |
|
| YONG, Y. |
ICAS 2002-1.9.1 |
SIMULATION OF STATISTICAL MEAN BEHAVIORS AND COHERENT STRUCTURES OF INCOMPRESSIBLE
TURBULENT FLOWS USING UNILATERAL-AVERAGE BASED GOVERNING EQUATIONS |
|
| YOSHIDA, K. |
ICAS 2002-2.8.1 |
EXPERIMENTAL AND NUMERICAL STUDY ON TRANSITION CHARACTERISTICS AT SUPERSONIC
SPEED |
|
| YU, S.D. |
ICAS 2002-4.2.1 |
FREE FLEXURAL VIBRATION OF RECTANGULAR PLATES HAVING SINGLE CRACKS |
|
| YUMASHEV, V.L. |
ICAS 2002-1.4.2 |
MULTIDISCIPLINARY OPTIMIZATION OF AIRCRAFT PARAMETERS BY THE LOCAL DISTRIBUTED
CRITERIA METHOD |
|
| ZAGAINOV, G.I. |
ICAS 2002-R72 |
GENERATION OF SU-27 FIGHTER |
|
| ZAIN, Z.M. |
ICAS 2002-R70 |
DESIGN ISSUES RELATING TO ULTRALIGHT HELICOPTERS WITH LARGE COMPOUND ROTORS
OPERATING IN GROUND EFFECT |
|
| ZAMMIT-MANGION, D. |
ICAS 2002-7.10.5 |
AN OPERATIONAL EVALUATION OF A TAKE-OFF PERFORMANCE MONITORING ALGORITHM |
|
| ZAN, S.J. |
ICAS 2002-3.11.1 |
WIND TUNNEL TESTING TO DETERMINE UNSTEADY LOADS ON A HELICOPTER FUSELAGE
IN A SHIP AIRWAKE |
|
| ZASUMA, M. |
ICAS 2002-7.4.4 |
SIMULATION OF TERRAIN REFERENCE NAVIGATION SYSTEM BASED ON IMAGE MATCHING
FROM DIGITAL VIDEO CAMERA |
|
| ZHAN, H. |
ICAS 2002-2.5.2 |
RECENT EXAMPLES ON DESIGN AERODYNAMICS FOR TRANSPORT AIRCRAFT |
|
| ZHANG, F. |
ICAS 2002-1.1.3 |
EVALUATION OF THREE DECOMPOSITION MDO ALGORITHMS |
|
| ZHANG, F. |
ICAS 2002-2.11.1 |
OPTIMIZATIONS OF AIRFOIL AND WING USING GENETIC ALGORITHM |
|
| ZHANG, G. |
ICAS 2002-6.3.3 |
A UNIQUE SPRAY FORMING PROCESS FOR HIGH TEMPERATURE MATERIALS FOR AEROSPACE
APPLICATIONS |
|
| ZHANG, H. |
ICAS 2002-2.1.4 |
A RAPID NUMERICAL METHOD FOR 3D AERO DYNAMICS DESIGN OF COMPRESSOR BLADE
ROW (APPLICATION TO A LOW SPEED EXPERIMENTAL MULTI-IDENTICAL-STAGE COMPRESSOR
DESIGN) |
|
| ZHANG, J. |
ICAS 2002-3.9.3 |
CONTROL OF CLOSED-TYPE SUPERSONIC CAVITY FLOWS |
|
| ZHANG, L. |
ICAS 2002-6.1.4 |
PROCESS MODELING AND REENGINEERING ON AIRCRAFT PRODUCT LIFECYCLE |
|
| ZHANG, X. |
ICAS 2002-R42 |
FATIGUE LIFE PREDICTION OF 3-D PROBLEMS BY DAMAGE MECHANICS WITH SPECTRUM
LOADING |
|
| ZHANG, Z.Y. |
ICAS 2002-2.4.2 |
INVESTIGATION OF HIGH-LIFT, MILD-STALL WINGS |
|
| ZHANG, Z.Y. |
ICAS 2002-2.5.2 |
RECENT EXAMPLES ON DESIGN AERODYNAMICS FOR TRANSPORT AIRCRAFT |
|
| ZHENGHONG, G. |
ICAS 2002-8.1.1 |
THE INVESTIGATION OF MULTI-DISCIPLINARY AND MULTI-OBJECTIVE OPTIMIZATION
METHOD FOR THE AIRCRAFT CONFIGURATION DESIGN |
|
| ZHU, B. |
ICAS 2002-1.10.4 |
NUMERICAL OPTIMIZATION DESIGN OF WINGS BY SOLVING ADJOINT EQUATIONS |
|
| ZHU, B. |
ICAS 2002-R53 |
NUMERICAL SIMULATION OF NAVIER-STOKES EQUATIONS FOR HELICOPTER ROTOR IN
FORWARD FLIGHT USING MOVING CHIMERA GRIDS |
|
| ZHU, K. |
ICAS 2002-P3 |
ANALYSIS OF PREVENTIVE MAINTENANCE PROGRAM IMPROVEMENT FOR IN-SERVICE
AIRCRAFT |
|
| ZHU, X. |
ICAS 2002-R80 |
APPLICATION OF FAULT DIAGNOSIS EXPERT SYSTEM FOR AIRCRAFT ELECTRIC POWER
SYSTEM |
|
| ZHUK, Y. |
ICAS 2002-3.1.2 |
FAILURE PREDICTION OF STRINGER STIFFENED COMPOSITE PANELS WITH IMPACT
DAMAGE UNDER UNIAXIAL COMPRESSION |
|
| ZIMCIK, D. |
ICAS 2002-4.3.3 |
SMART SPRING CONCEPT FOR HELICOPTER VIBRATION AND NOISE CONTROL |
|
| ZINGG, D.W. |
ICAS 2002-1.7.3 |
FROM ANALYSIS TO DESIGN OF HIGH-LIFT CONFIGURATIONS USING A NEWTON-KRYLOV
ALGORITHM |
|
| ZINGG, D.W. |
ICAS 2002-1.9.3 |
A FULLY COUPLED NEWTON-KRYLOV SOLVER FOR TURBULENT AERODYNAMIC FLOWS |
|
| ZINGG, D.W. |
ICAS 2002-6.6.2 |
DEVELOPING A NEW FLAP FOR A LIGHT UTILITY TRANSPORT AIRPLANE |
|
| ZLOCKA, M. |
ICAS 2002-5.5.3 |
A STUDY OF FLIGHT DYNAMICS AND AUTOMATIC CONTROL OF AN ANIMALOPTER |
|
| ZWEBER, J.V. |
ICAS 2002-4.4.5 |
INVESTIGATION OF SHOCK-INDUCED LCO OF A WING/STORE CONFIGURATIONUSING
THE TRANSONIC SMALL DISTURBANCE METHOD |
|