Name |
Title |
ICAS Paper Number |
Abbott K. H. |
FUTURE FLIGHT DECKS |
ICAS-98-1.9.3 |
Abbott T. S. |
FUTURE FLIGHT DECKS |
ICAS-98-1.9.3 |
Abidogun K. |
THE FLOWFIELD CHARACTERISTICS OF A CONFINED SWIRLING FLOW |
ICAS-98-R.5.9 |
Adibroto A. |
COMMEMORATING TEN YEARS OPERATION OF THE INDONESIAN LOW SPEED TUNNEL (ILST) |
ICAS-98-3.11.3 |
Afnaim S. |
FATIGUE AND DAMAGE TOLERANCE SUBSTANTIATION OF THE GALAXY EXECUTIVE JET AIRCRAFT |
ICAS-98-5.7.3 |
Agrell J. |
AERODYNAMIC CHARACTERISTICS OF MISSILES WITH TRIANGULAR CROSS SECTIONS |
ICAS-98-3.6.3 |
Agrell N. |
COMPUTATION OF WIND TUNNEL FLOWS IN TRANSONIC SLOTTED-WALL TEST SECTIONS |
ICAS-98-3.11.1 |
Ahmed N. A. |
EXPERIMENTAL INVESTIGATION OF AXIAL COMPRESSOR CASCADE PERFORMANCE UNDER THE INFLUENCE OF LOW INTENSITY TURBULENCE |
ICAS-98-5.4.5 |
Ahmed N. A. |
IMPROVING THE AERODYNAMIC EFFICIENCY OF A WING BY ACOUSTIC EXCITATION |
ICAS-98-3.9.4 |
Ahmed S. A. |
THE FLOWFIELD CHARACTERISTICS OF A CONFINED SWIRLING FLOW |
ICAS-98-R.5.9 |
Allen C. B. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Allerton D. J. |
A DISTRIBUTED APPROACH TO THE DESIGN OF A REAL-TIME ENGINEERING FLIGHT SIMULATOR |
ICAS-98-1.1.2 |
Allerton D. J. |
ROUTING ALGORITHMS FOR REAL-TIME MISSION MANAGEMENT |
ICAS-98-6.2.3 |
Alonso A. C. P. |
BRAZILIAN F-S EXTERNAL STORES AEROELASTIC INTEGRATION |
ICAS-98-4.5.2 |
Altman A. |
DESIGN METHODOLOGY FOR LOW SPEED HIGH ALTITUDE LONG ENDURANCE UNMANNED AERIAL VEHICLES |
ICAS-98-7.6.3 |
Amato M. |
EULER /NAVIER-STOKES SIMULATION FOR PROPULSION-AIRFRAME INTEGRATION OF ADVANCED PROPELLER-DRIVEN AIRCRAFT IN THE EUROPEAN RESEARCH PROGRAMS GEMINI/ APIAN |
ICAS-98-5.10.2 |
Amiryants G. A. |
ADAPTIVE SELECTIVELY-DEFORMABLE STRUCTURES; NEW CONCEPT IN ENGINEERING |
ICAS-98-6.8.3 |
Amphlett T. |
MAXIMISING THE EFFICIENCY OF THE STRUCTURAL QUALIFICATION PROCESS |
ICAS-98-6.8.1 |
Andersen G. |
CONTROL SURFACE EFFECTIVENESS IN THE TRANSONIC REGIME |
ICAS-98-4.6.4 |
Anderson S. B. |
HUMAN FACTORS ASPECTS OF REMOTELY PILOTED AIRCRAFT |
ICAS-98-6.3.4 |
Anghileri M. |
CRASH BEHAVIOUR OF HELICOPTER FUEL TANK STRUCTURES |
ICAS-98-4.2.1 |
Anglada M. |
THE EVOLUTION UNDER STRESS OF THE SUPERALLOY / PROTECTIVE COATING INTERFACE |
ICAS-98-4.2.2 |
Annes da Silva R. G. |
BRAZILIAN F-S EXTERNAL STORES AEROELASTIC INTEGRATION |
ICAS-98-4.5.2 |
Arbuckle P. D. |
FUTURE FLIGHT DECKS |
ICAS-98-1.9.3 |
Archer R. D. |
IMPROVING THE AERODYNAMIC EFFICIENCY OF A WING BY ACOUSTIC EXCITATION |
ICAS-98-3.9.4 |
Arendsen P. |
FROM A MONO-DISCIPLINARY TO A MULTI-DISCIPLINARY APPROACH IN AEROSPACE: AS SEEN FROM AN INFORMATION AND COMMUNICATION TECHNOLOGY PERSPECTIVE |
ICAS-98-6.8.2 |
Arnott D. R. |
BOND DURABILITY PERFORMANCE -THE AUSTRALIAN SILANE SURFACE TREATMENT |
ICAS-98-5.3.1 |
Asai K. |
LUMINESCENT PAINT TECHNOLOGY FOR TEMPERATURE AND PRESSURE MEASUREMENTS IN A CRYOGENIC WIND TUNNEL |
ICAS-98-3.3.1 |
Astarita T. |
HEAT TRANSFER MEASUREMENTS IN A ROTATING CHANNEL |
ICAS-98-5.4.1 |
Auld D. J. |
DIRECT SIMULATION (MONTE CARLO) OF DELTA WINGS IN THREE-DIMENSIONAL, NEAR-CONTINUUM, SUBSONIC FLOWS |
ICAS-98-R.2.2 |
Azevedo J. L. F. |
ADAPTIVE MESH REFINEMENT ON THE SOLUTION OF TWO-DIMENSIONAL VISCOUS AEROSPACE PROBLEMS |
ICAS-98-2.2.3 |
Azevedo J. L. F. |
AXISYMETRIC SIMULATIONS OF TURBULENT COMPRESSIBLE FLOWS OVER AEROSPACE VEHICLES |
ICAS-98-2.8.3 |
Azevedo J. L. F. |
THREE DIMENSIONAL FLOW SIMULATION IN THE TEST SECTION OF A SLOTTED TRANSONIC WIND TUNNEL |
ICAS-98-R.3.11 |
Babuev V. P. |
EXPERIMENTAL INVESTIGATION ON THE APPLICATION OF HYBRID LAMINAR FLOW CONTROL TO LARGE-SCALE SWEPT WING MODELS AT SUBSONIC SPEEDS |
ICAS-98-3.4.2 |
Bader M. |
THE EFFECT OF MATRIX MOISTURE CONTENT ON THE REPAIR OF CARBON FIBRE REINFORCED EPOXY |
ICAS-98-4.4.3 |
Bahadori M. Y. |
CHARACTERISTICS OF MOMENTUM-DOMINATED HYDROCARBON TURBULENT DIFFUSION FLAMES |
ICAS-98-5.8.1 |
Baker A. A. |
BOND DURABILITY PERFORMANCE -THE AUSTRALIAN SILANE SURFACE TREATMENT |
ICAS-98-5.3.1 |
Baker A. A. |
THROUGH-THICKNESS STRESSES IN AIRCRAFT BONDED JOINTS |
ICAS-98-4.3.4 |
Balan M. |
FINITE ELEMENT MODELING AND EXPERIMENTAL STUDY OF A GAS TURBINE ENGINE BLADE UNDER BIAXIAL LOADING |
ICAS-98-5.1.4 |
Baldonado M. |
TESTING OF AN AUTOMATIC, LOW ALTITUDE, ALL TERRAIN GROUND COLLISION AVOIDANCE SYSTEM |
ICAS-98-1.8.1 |
Bandara S. N. |
INTEGRATED FLIGHT AND PAYLOAD CONTROL FOR DIRECTIONAL PAYLOADS ON UAVS |
ICAS-98-3.7.2 |
Bannister M. |
COMPRESSIONS AFTER IMPACT BEHAVIOUR OF MULTILAYER WOVEN GLASS/VINYL ESTER COMPOSITES |
ICAS-98-5.9.1 |
Barfield A. F. |
RESULTS OF A JOINT US/SWEDISH AUTO GROUND COLLISION AVOIDANCE SYSTEM PROGRAM |
ICAS-98-1.8.2 |
Barnes T. J. |
EVOLUTION OF TRANSPORT AIRPLANE STRUCTURAL DESIGN CRILERIA TO INCORPORATE ADVANCES IN TECHNOLOGY |
ICAS-98-4.7.3 |
Bartholomeusz R. A. |
THROUGH-THICKNESS STRESSES IN AIRCRAFT BONDED JOINTS |
ICAS-98-4.3.4 |
Basso E. |
THREE DIMENSIONAL FLOW SIMULATION IN THE TEST SECTION OF A SLOTTED TRANSONIC WIND TUNNEL |
ICAS-98-R.3.11 |
Bathory Z. |
ANALYSIS OF AIRCRAFT STOCHASTIC MOTION AFTER LOSING THE CONTROL |
ICAS-98-7.5.1 |
Battipede M. |
AN ADAPTATIVE NEUROCONTROLLER FOR A NON-LINEAR HELICOPTER MODEL |
ICAS-98-7.1.4 |
Bayrak S. |
EXPERIMENTAL INVESTIGATION OF A DIFFUSER FOR COOLING AND AIR CONDITIONING SYSTEM |
ICAS-98-7.6.2 |
Bayramgil V. |
EXPERIMENTAL INVESTIGATION OF A DIFFUSER FOR COOLING AND AIR CONDITIONING SYSTEM |
ICAS-98-7.6.2 |
Becker K. |
MEGAFLOW -A NUMERICAL FLOW SIMULATION SYSTEM |
ICAS-98-2.7.4 |
Belo E. M. |
IDENTIFICATION OF AIRCRAFT NON-LINEAR DYNAMICS USING VOLTERRA SERIES |
ICAS-98-1.10.5 |
Belov I. F. |
ANALYTICAL AND EXPERIMENTAL INVESTIGATIONS OF AN IMPROVED AERODYNAMIC ORBITER CONFIGURATION |
ICAS-98-R.1.2 |
Belton W. A |
A TOOLSET FOR THE DESIGN OF AUTONOMOUS UAV SYSTEMS |
ICAS-98-3.7.3 |
Bengin A. |
RELIABILITY EVALUATION OF AEROSPACE COMPONENTS |
ICAS-98-7.1.3 |
Bengin A. |
THREE DIMENSIONAL ROTOR FLOW CALCULATION |
ICAS-98-7.4.5 |
Bennani S. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN. PART I : ?-ANALYSIS OF DESIGN ENTRIES TO A ROBUST FLIGHT CONTROL BENCHMARK |
ICAS-98-1.6.1 |
Beran P. |
CONTROL SURFACE EFFECTIVENESS IN THE TRANSONIC REGIME |
ICAS-98-4.6.4 |
Berglind T. |
A MULTIGRID ALGORITHM FOR INVISCID FLOW COMPUTATIONS ON UNSTRUCTURED GRIDS |
ICAS-98-2.7.3 |
Berkes U. L. |
DESIGN AND VERIFICATION PHILOSOPHIES FOR HIGH PERFORMANCE AEROSPACE VEHICLE STRUCTURES UNDER COMBINED MECHANICAL AND THERMAL LOADING |
ICAS-98-1.2.2 |
Bernadou J. -P. |
THE EVOLUTION UNDER STRESS OF THE SUPERALLOY / PROTECTIVE COATING INTERFACE |
ICAS-98-4.2.2 |
Berton E. |
3D BOUNDARY-LAYER ON ROTATING WINGS: EXPERIMENTS AND CALCULATIONS |
ICAS-98-3.1.1 |
Beyers M. E. |
CONSIDERATIONS IN APPLYING MILITARY AIRCRAFT FOREBODY FLOW CONTROL METHODOLOGY TO COMMERCIAL AIRCRAFT |
ICAS-98-3.4.5 |
Beyers M. E. |
EFFECT OF LEX SURFACES ON LATERAL-DIRECTIONAL DYNAMIC STABILITY OF COMBAT AIRCRAFT |
ICAS-98-1.4.2 |
Bhattacharya A. K. |
UNSTEADY TRANSONIC HYBRID INTEGRAL-EQUATION / FINITE-VOLUME SCHEME FOR TRAJECTORY SIMULATION OF STORES WITH TIME-STEP ADAPTATION |
ICAS-98-2.4.4 |
Biedermann 0. |
MORE EFFICIENT FLUID POWER SYSTEMS USING VARIABLE DISPLACEMENT HYDRAULIC MOTORS |
ICAS-98-5.5.1 |
Bil C. |
A TOOLSET FOR THE DESIGN OF AUTONOMOUS UAV SYSTEMS |
ICAS-98-3.7.3 |
Bil C. |
INTEGRATED FLIGHT AND PAYLOAD CONTROL FOR DIRECTIONAL PAYLOADS ON UAVS |
ICAS-98-3.7.2 |
Bil C. |
UAVS OVER AUSTRALIA: CAPABILITIES AND OPPORTUNITIES |
ICAS-98-3.7.5 |
Bircher T. |
DEVELOPMENT, QUALIFICATION AND FLIGHT TESTING OF A WINGGRID ON A JET-POWERED TESTBED |
ICAS-98-1.1.4 |
Bisagni C. |
BUCKLING TESTS OF CARBON-EPOXY LAMINATED CYLINDRICAL SHELLS UNDER AXIAL COMPRESSION AND TORSION |
ICAS-98-4.4.1 |
Blanchard R. C. |
MARS ENTRY VEHICLE AERODYNAMIC FLIGHT MEASUREMENTS |
ICAS-98-1.2.3 |
Blaschke R. C. |
EXPERIMENTAL AND NUMERICAL INVESTIGATIONS ON WAVERIDERS IN DIFFERENT FLIGHT REGIMES |
ICAS-98-2.1.4 |
Boelens O. J. |
INVESTIGATION INTO THE FORMATION OF WAVES ON THIN LAYERS OF DE-/ ANTI-ICING FLUIDS ON WINGS |
ICAS-98-7.1.1 |
Boermans L. M. M. |
AERODYNAMIC DESIGN OF HIGH-PERFORMANCE SAILPLANE WING-FUSELAGE COMBINATIONS |
ICAS-98-2.9.2 |
Bokser V. D. |
EXPERIMENTAL INVESTIGATION ON THE APPLICATION OF HYBRID LAMINAR FLOW CONTROL TO LARGE-SCALE SWEPT WING MODELS AT SUBSONIC SPEEDS |
ICAS-98-3.4.2 |
Bolsunovsky A. L. |
RECENT INVESTIGATIONS OF THE VERY LARGE PASSENGER BLENDED-WING-BODY AIRCRAFT |
ICAS-98-4.10.2 |
Bond D. |
THE EFFECT OF MATRIX MOISTURE CONTENT ON THE REPAIR OF CARBON FIBRE REINFORCED EPOXY |
ICAS-98-4.4.3 |
Bones C. A. |
BRAZILIAN F-S EXTERNAL STORES AEROELASTIC INTEGRATION |
ICAS-98-4.5.2 |
Boniface J.-C. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Borello L. |
MECHANICAL FAILURES OF FLAP CONTROL SYSTEMS AND RELATED MONITORING TECHNIQUES |
ICAS-98-5.5.2 |
Borowiczyk H. |
THE NEURAL DIAGNOSTIC METHOD AND A COMPLEX SYSTEM OF DIAGNOSING AIRFRAME AND POWERPLANT |
ICAS-98-6.6.4 |
Bose S. |
CAPABILITIES OF SURFACE MEASUREMENT TECHNIQUES AND THEIR IMPACT ON MODERN WING-DESIGN AND ASSESSMENT |
ICAS-98-3.3.4 |
Bousson K. |
FUZZY STABILITY AUGMENTATION SYSTEM FOR AIRCRAFT HANDLING QUALITIES |
ICAS-98-1.10.4 |
Boyle F. |
EULER /NAVIER-STOKES SIMULATION FOR PROPULSION-AIRFRAME INTEGRATION OF ADVANCED PROPELLER-DRIVEN AIRCRAFT IN THE EUROPEAN RESEARCH PROGRAMS GEMINI/ APIAN |
ICAS-98-5.10.2 |
Braithwaite G. R. |
A SYSTEMATIC INVESTIGATION INTO AUSTRALIAN AVIATION SAFETY |
ICAS-98-1.9.1 |
Bramley K. |
PERFORMANCE FLIGHT TESTING OF AN F-111 C AIRCRAFT |
ICAS-98-1.1.1 |
Brandao M. P. |
BRAZILIAN F-S EXTERNAL STORES AEROELASTIC INTEGRATION |
ICAS-98-4.5.2 |
Brannstrom B. |
RESULTS OF A JOINT US/SWEDISH AUTO GROUND COLLISION AVOIDANCE SYSTEM PROGRAM |
ICAS-98-1.8.2 |
Bray T. P. |
PREDICTION OF THE VORTICITY FIELD PRODUCED BY AIR-JET VORTEX GENERATORS |
ICAS-98-2.8.2 |
Breitsamter C. |
VORTICAL FLOWFIELD STRUCTURE AT FORWARD SWEPT WING CONFIGURATIONS |
ICAS-98-3.8.2 |
Brenner M. J. |
ON - LINE ROBUST MODAL STABILILY PREDICTION USING WAVELET PROCESSING |
ICAS-98-4.9.1 |
Brian G. |
PERFORMANCE FLIGHT TESTING OF AN F-111 C AIRCRAFT |
ICAS-98-1.1.1 |
Brocas D. |
CLOSED-LOOP CONSTRAINED CONTROL ALLOCATION FOR A SUPERMANOEUVERABLE AIRCRAFT |
ICAS-98-1.10.2 |
Brot A. |
FATIGUE AND DAMAGE TOLERANCE SUBSTANTIATION OF THE GALAXY EXECUTIVE JET AIRCRAFT |
ICAS-98-5.7.3 |
Brown J. |
FINITE ELEMENT MODELING AND EXPERIMENTAL STUDY OF A GAS TURBINE ENGINE BLADE UNDER BIAXIAL LOADING |
ICAS-98-5.1.4 |
Bruno A. E. |
AN IMPROVED TECHNIQUE FOR FLIGHT PATH AND GROUNDSPEED ANALYSIS USING RECORDED RADAR DALA |
ICAS-98-6.5.3 |
Budd G. D. |
PREDICTED DEEP-STALL FLIGHT CHARACTERISTICS OF TWO HYPERSONIC FLIGHT VEHICLES |
ICAS-98-1.3.2 |
Buffardi R. |
SAFETY ASSESSMENT OF AIRCRAFT MOUNTED SYSTEMS |
ICAS-98-6.7.3 |
Bulbeck C. J. |
AN ENGINEERING METHODOLOGY FOR SUBSONIC STORE TRAJECTORY PREDICTION |
ICAS-98-2.10.3 |
Buonomo C. A. |
AXISYMETRIC SIMULATIONS OF TURBULENT COMPRESSIBLE FLOWS OVER AEROSPACE VEHICLES |
ICAS-98-2.8.3 |
Burgsmueller W. |
ENGINE INTEGRATION ON FUTURE TRANSPORT AIRCRAFT - THE EUROPEAN RESEARCH PROGRAMMES DUPRIN/ENIFAIR |
ICAS-98-5.6.1 |
Buzoverya N. P. |
RECENT INVESTIGATIONS OF THE VERY LARGE PASSENGER BLENDED-WING-BODY AIRCRAFT |
ICAS-98-4.10.2 |
Byzov V. N. |
FLIGHT RESEARCHES OF VISCOSITY INFLUENCE ON SHARP CONES AERODYNAMICAL CHARACTERISTICS IN HYPERSONIC LOW DENSITY FLOW |
ICAS-98-R.3.3 |
Cafarelli R. |
ENGINE SUB-IDLE MODEL |
ICAS-98-5.6.2 |
Callinan R. J. |
ANALYSIS OF THE INTERACTION EFFECT FOR BONDED REPAIRS |
ICAS-98-R.5.3 |
Callinan R. J. |
DEVELOPMENT OF AN ANALYTICAL EXPRESSION AND A FINITE ELEMENT PROCEDURE TO DETERMINE THE RESIDUAL STRESSES IN BONDED REPAIRS |
ICAS-98-4.8.3 |
Callinan R. J. |
OPTIMIZATION OF A COMPOSITE BONDED REPAIR TO CRACKED PANELS SUBJECTED TO ACOUSTIC EXCITATION |
ICAS-98-5.3.2 |
Callus P. |
COMPRESSIONS AFTER IMPACT BEHAVIOUR OF MULTILAYER WOVEN GLASS/VINYL ESTER COMPOSITES |
ICAS-98-5.9.1 |
Camelier I. A. |
A PASSIVE AERODYNAMIC STABILIZATION SYSTEM OF SATELLITES FOR LOW EARTH ORBIT: AN ANALYTICAL APPROACH |
ICAS-98-1.3.4 |
Campanile L. F. Hanselka H. |
A LIGHTWEIGHT CONCEPT FOR AERODYNAMIC SURFACES WITH VARIABLE CAMBER |
ICAS-98-4.11.3 |
Campos L. M. B. C. |
AN ANALYTICAL APPROACH TO HIGH-ORDER, NON LINEAR AIRPLANE STABILITY PROBLEMS |
ICAS-98-R.1.7.1 |
Cardascia L. |
OPTIMAL PLACEMENT OF PIEZOELECTRIC SENSORS AND ACTUATORS USING COMBINATORIAL OPTIMISATION |
ICAS-98-4.11.2 |
Cardone G. |
HEAT TRANSFER MEASUREMENTS IN A ROTATING CHANNEL |
ICAS-98-5.4.1 |
Carlomagno G. M. |
HEAT TRANSFER MEASUREMENTS IN A ROTATING CHANNEL |
ICAS-98-5.4.1 |
Casalis G. |
STABILITY ANALYSIS BY THE OS AND PSE APPROACHES: COMPARISONS WITH EXPERIMENTS |
ICAS-98-2.8.1 |
Casseta O. P. |
HUMAN FACTORS MODELS AND CLASSIFICATION SCHEMES FOR IMPROVING OCCURENT DATA REPORTING SYSTEMS |
ICAS-98-1.9.4 |
Caston C. |
AERODYNAMIC INTEGRATION OF HIGH SPEED PROPELLER ON AIRCRAFT: RECENT INVESTIGATIONS IN EUROPEAN WIND TUNNELS |
ICAS-98-5.10.3 |
Catalano F. M. |
VISCOUS DRAG OPTIMIZATION FOR A TRANSPORT AIRCRAFT MISSION ADAPTIVE WING |
ICAS-98-2.3.2 |
Caves R. E. |
A SYSTEMATIC INVESTIGATION INTO AUSTRALIAN AVIATION SAFETY |
ICAS-98-1.9.1 |
Caves R. E. |
DEVELOPMENT OF AN INTEGRATED CONCEPTUAL AIRCRAFT DESIGN AND AIRCRAFT NOISE MODEL FOR CIVIL TRANSPORT AIRCRAFT |
ICAS-98-6.4.3 |
Caves R. E. |
ESTIMATION OF CIVIL AIRCRAFT PERFORMANCE AND OPERATING PRACTICES FROM RADAR DATA |
ICAS-98-5.11.1 |
Caves R. E. |
THE RISKS OF OVERRUNS |
ICAS-98-1.11.1 |
Cawood M. |
RESULTS OF A JOINT US/SWEDISH AUTO GROUND COLLISION AVOIDANCE SYSTEM PROGRAM |
ICAS-98-1.8.2 |
Cenko A. |
ACFD APPLICATIONS TO STORE SEPARATION |
ICAS-98-2.10.4 |
Chen M. Z. |
A NEW PROCEDURE FOR SIMULATING ROTOR/STATOR INTERACTION IN TURBOMACHINERY |
ICAS-98-7.4.3 |
Chen S. |
APPLICATION OF AN IMPROVED KˇE MODEL TO SEPARATION FLOWS |
ICAS-98-3.10.1 |
Chen Y. |
RESEARCH OF ACTIVE VIBRATION CONTROL TECHNOLOGIES FOR A COMPOSITE SHELL |
ICAS-98-4.11.1 |
Cheng G. M. |
EFFECTS OF STRETCHING-BENDING COUPLINGS ON THE BUCKLING AND THERMAL BUCKLING BEHAVIOR OF UNSYMMETRIC LAMINATES |
ICAS-98-4.8.2 |
Chester D. H. |
REVISED EQUATION FOR TIRE LATERAL DYNAMICS IN SHIMMY MOTION |
ICAS-98-P1 |
Chester R. J. |
BOND DURABILITY PERFORMANCE -THE AUSTRALIAN SILANE SURFACE TREATMENT |
ICAS-98-5.3.1 |
Chester R. J. |
THROUGH-THICKNESS STRESSES IN AIRCRAFT BONDED JOINTS |
ICAS-98-4.3.4 |
Chiappa C. |
FLEXIBLE STRUCTURE CONTROL BY MODAL MULTI-MODEL APPROACH: APPLIED TO FLEXIBLE AIRCRAFT |
ICAS-98-1.5.2 |
Chiesa S. |
LIFE CYCLE COST ESTIMATION TOOL FOR CONCEPTUAL DESIGN |
ICAS-98-6.1.2 |
Chiu W. K. |
OPTIMIZATION OF A COMPOSITE BONDED REPAIR TO CRACKED PANELS SUBJECTED TO ACOUSTIC EXCITATION |
ICAS-98-5.3.2 |
Choi S. |
USE OF CFD FOR DESIGN VALIDATION OF A TRANSONIC CIVIL TRANSPORT |
ICAS-98-2.3.3 |
Chu J. K. |
AERODYNAMIC DESIGN OPTIMISATION APPLIED TO CIVIL TRANSPORTS WITH UNDERWING MOUNTED ENGINES |
ICAS-98-2.3.1 |
Clark G. |
THE INFLUENCE OF CORROSION ON AIRCRAFT STRUCTURAL INTEGRITY |
ICAS-98-5.2.1 |
Coiro D. P. |
NUMERICAL, WIND-TUNNEL AND FLIGHT TESTS FOR P92J AND P96 LIGHT AIRCRAFT |
ICAS-98-3.11.2 |
Cole G. |
THE INFLUENCE OF CORROSION ON AIRCRAFT STRUCTURAL INTEGRITY |
ICAS-98-5.2.1 |
Collongo C. |
TB 20, A LOW COST TOOL FOR IN-FLIGHT TEACHING |
ICAS-98-P2 |
Conser D. P. |
DYNAMIC LOAD DEVELOPMENT AND RESULTS FOR DYNAMIC EXCITATION OF A FULL-SCALE F/A-18 FATIGUE TEST ARTICLE |
ICAS-98-4.5.1 |
Cook R. |
THE INFLUENCE OF CORROSION ON THE FATIGUE AND FRACTURE BEHAVIOUR OF 7050-T76 ALUMINIUM ALLOY SPECIMENS CONTAINING COLD EXPANDED HOLES |
ICAS-98-5.2.2 |
Coton F. N. |
A STUDY OF VORTEX BREAKDOWN ON PITCHING DELTA WINGS USING HIGH RESOLUTION PRESSURE MEASUREMENTS |
ICAS-98-3.2.3 |
Coton P. |
STUDY OF ENVIRONMENT EFFECTS BY MEANS OF SCALE MODEL FLIGHT TESTS IN A LABORATORY |
ICAS-98-3.9.1 |
Crawford C. A. |
THE IMPACT OF ENGINE TECHNOLOGY ADVANCEMENTS ON THE RANGE V PERFORMANCE TRADE-OFF FOR A FUTURE COMBAT AIRCRAFT |
ICAS-98-1.10.1 |
Crenon P. |
ONERA ACTIVITIES ON SUPERSONIC TRANSPORT AIRCRAFT AERODYNAMICS |
ICAS-98-2.1.2 |
Cursolle J. P. |
HMD OFF-BORESIGHT SYMBOLOGY FOR FIXED-WINGS AIRCRAFT: AN EXPERIMENTAL APPROACH |
ICAS-98-6.3.1 |
Cvetkovic D. |
SIMULATION OF SPIN ON THE VUK-T SAILPLANE |
ICAS-98-P3 |
Czarnocki P. |
SOME INVESTIGATIONS ON WOOD-COMPOSITE STRUCTURES FOR VERY LIGHT AIRCRAFT (VLA) |
ICAS-98-4.4.4 |
Da Silva C. B. |
LARGE-EDDY SIMULATION OF A TRAILING VORTEX SYSTEM BEHIND A CIVIL AIRCRAFT MODEL |
ICAS-98-2.10.2 |
D'Alascio A. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Damilano J. G. |
STRUCTURAL DYNAMIC ANALYSIS OF NON-LINEAR MULTIBODY SYSTEMS BY A TIME-DISCONTINUOUS GALERKIN FINITE ELEMENT FORMULATION |
ICAS-98-4.9.4 |
Danehy P. M. |
INSTANTANEOUS PLIF MEASUREMENT OF SPECIES MOLE-FRACTION IN A VARYING TEMPERATURE SUPERSONIC FLOW |
ICAS-98-3.1.4 |
Danehy P. M. |
PLIF IMAGING OF THE SEPARATED REGION BEHIND A CONE IN A HYPERSONIC FLOW |
ICAS-98-3.10.4 |
Dang-Vu B. |
CLOSED-LOOP CONSTRAINED CONTROL ALLOCATION FOR A SUPERMANOEUVERABLE AIRCRAFT |
ICAS-98-1.10.2 |
Dardenne I. |
DESIGN OF FLIGHT CONTROL SYSTEM FOR A HIGHLY FLEXIBLE AIRCRAFT USING CONVEX SYNTHESIS |
ICAS-98-1.5.1 |
Darida M. |
WIND TUNNEL LNVESTIGATIONS ON RPV WING GLOVE CONFIGURATION |
ICAS-98-3.7.4 |
Davis M. J. |
BOND DURABILITY PERFORMANCE -THE AUSTRALIAN SILANE SURFACE TREATMENT |
ICAS-98-5.3.1 |
de Castro Santos L. C. |
UNSTEADY PARALLEL AIRFOIL DESIGN FOR ROTARY WING APPLICATIONS |
ICAS-98-2.5.2 |
de Feria Mello O. A. |
BRAZILIAN F-S EXTERNAL STORES AEROELASTIC INTEGRATION |
ICAS-98-4.5.2 |
De Medeiros M.A.F. |
NONLINEAR EVOLUTION OF A THREE-DIMENSIONAL WAVETRAIN IN A FLAT PLATE BOUNDARY LAYER |
ICAS-98-3.1.3 |
de Muynck R. J. |
COCKPIT SYSTEMS REQUIREMENTS IN A FUTURE ATM ENVIRONMENT |
ICAS-98-6.2.2 |
De Ponte S. |
SKIN FRICTION MEASUREMENTS DOWNSTREAM OF A BACK-FACING STEP |
ICAS-98-3.10.3 |
Delaurentis D. A. |
A STOCHASTIC DESIGN APPROACH FOR AIRCRAFT AFFORDABILITY |
ICAS-98-6.1.3 |
Denisov V. E. |
RECENT INVESTIGATIONS OF THE VERY LARGE PASSENGER BLENDED-WING-BODY AIRCRAFT |
ICAS-98-4.10.2 |
Deparis M. |
3D BOUNDARY-LAYER ON ROTATING WINGS: EXPERIMENTS AND CALCULATIONS |
ICAS-98-3.1.1 |
Dido F. |
DIAGNOSTIC FROM SYSTEM MODELS: THE ADAM EXPERT SYSTEM APPROACH |
ICAS-98-6.6.2 |
Dinkelmann M. |
OPTIMAL THREE-DIMENSIONAL RANGE CRUISE OF A DUAL-FUEL HYPERSONIC VEHICLE |
ICAS-98-1.3.1 |
Djojodihardjo H. |
N-2S0 PROTOTYPE 1 FLIGHT FLUTTER TESTING DEVELOPMENT |
ICAS-98-4.5.3 |
Doll C. |
FLEXIBLE STRUCTURE CONTROL BY MODAL MULTI-MODEL APPROACH: APPLIED TO FLEXIBLE AIRCRAFT |
ICAS-98-1.5.2 |
Doll C. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN PART 2: EVALUATION OF A NEW TOOL FOR ?-ANALYSIS |
ICAS-98-1.6.2 |
Drack L. E. |
DESIGN AND ANALYSIS OF PROPELLERS FOR GENERAL AVIATION AIRCRAFT NOISE REDUCTION |
ICAS-98-5.11.3 |
Duarte J. A. A. |
STRUCTURAL DYNAMIC ANALYSIS OF NON-LINEAR MULTIBODY SYSTEMS BY A TIME-DISCONTINUOUS GALERKIN FINITE ELEMENT FORMULATION |
ICAS-98-4.9.4 |
Dubuc L. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Dumas A. |
AERODYNAMIC INTEGRATION OF HIGH SPEED PROPELLER ON AIRCRAFT: RECENT INVESTIGATIONS IN EUROPEAN WIND TUNNELS |
ICAS-98-5.10.3 |
Dunn S. A. |
OPTIMISATION OF THE STRUCTURAL DYNAMIC FINITE-ELEMENT MODEL FOR A COMPLETE AIRCRAFT |
ICAS-98-4.9.3 |
Duprat D. |
AN IMPROVED FATIGUE APPROACH FOR DESIGNING AIRCRAFT JOINTS |
ICAS-98-5.3.4 |
Duveau R. |
ONERA ACTIVITIES ON SUPERSONIC TRANSPORT AIRCRAFT AERODYNAMICS |
ICAS-98-2.1.2 |
Eastep F. |
CONTROL SURFACE EFFECTIVENESS IN THE TRANSONIC REGIME |
ICAS-98-4.6.4 |
Eaton J. A. |
EULER /NAVIER-STOKES SIMULATION FOR PROPULSION-AIRFRAME INTEGRATION OF ADVANCED PROPELLER-DRIVEN AIRCRAFT IN THE EUROPEAN RESEARCH PROGRAMS GEMINI/ APIAN |
ICAS-98-5.10.2 |
Eggers T. |
EXPERIMENTAL AND NUMERICAL INVESTIGATIONS ON WAVERIDERS IN DIFFERENT FLIGHT REGIMES |
ICAS-98-2.1.4 |
Eliasson P. |
ACCURACY OF UNSTEADY TRANSONIC FLOW COMPUTATIONS |
ICAS-98-2.4.2 |
Eliasson P. |
PROPELLER SLIPSTREAM COMPUTATIONAL METHODS |
ICAS-98-2.6.2 |
Engelhardt J. |
MORE EFFICIENT FLUID POWER SYSTEMS USING VARIABLE DISPLACEMENT HYDRAULIC MOTORS |
ICAS-98-5.5.1 |
Ericsson L. E. |
CONSIDERATIONS IN APPLYING MILITARY AIRCRAFT FOREBODY FLOW CONTROL METHODOLOGY TO COMMERCIAL AIRCRAFT |
ICAS-98-3.4.5 |
Ericsson L. E. |
EFFECT OF LEX SURFACES ON LATERAL-DIRECTIONAL DYNAMIC STABILITY OF COMBAT AIRCRAFT |
ICAS-98-1.4.2 |
Erim M. Z. |
EXPERIMENTAL INVESTIGATION OF A DIFFUSER FOR COOLING AND AIR CONDITIONING SYSTEM |
ICAS-98-7.6.2 |
Erkara S. |
EXPERIMENTAL INVESTIGATION OF LOCKED VORTEX STRUCTURES FOR DRAG REDUCTION OF BLUNT BODIES |
ICAS-98-P4 |
Eussen B. J. G. |
COMPREHENSIVE TIME ANALYSIS IN AEROELASTIC SIMULATIONS |
ICAS-98-4.3.3 |
Eve 0. |
NUMERICAL MODELLING FOR PREDICTING DAMAGE TOLERANCE OF COMPOSITE STRUCTURE |
ICAS-98-5.9.3 |
Ewing M. |
PREDICTION OF ANTISYMMETRIC BUFFET LOADS ON HORIZONTAL STABILIZERS IN MASSIVELY SEPARATED FLOWS |
ICAS-98-4.1.1 |
Eyi S. |
TURBOMACHINERY BLADE DESIGN USING THE NAVIER-STOKES EQUATIONS |
ICAS-98-5.4.4 |
Fairlie B. D. |
AN ENGINEERING METHODOLOGY FOR SUBSONIC STORE TRAJECTORY PREDICTION |
ICAS-98-2.10.3 |
Falzon P. J. Herszberg I. |
STRENGTH PREDICTION OF 2-D BRAIDED CARBON/EPOXY COMPOSITES |
ICAS-98-4.8.1 |
Fang W. |
STUDY OF WING STRUCTURAL LAYOUT DECISION SUPPORT SYSTEM |
ICAS-98-4.7.4 |
Farokhi S. |
PREDICTION OF ANTISYMMETRIC BUFFET LOADS ON HORIZONTAL STABILIZERS IN MASSIVELY SEPARATED FLOWS |
ICAS-98-4.1.1 |
Faulkner J. P. E. |
A SYSTEMATIC INVESTIGATION INTO AUSTRALIAN AVIATION SAFETY |
ICAS-98-1.9.1 |
Favier D. |
3D BOUNDARY-LAYER ON ROTATING WINGS: EXPERIMENTS AND CALCULATIONS |
ICAS-98-3.1.1 |
Fedunov B. E. |
ON-BOARD OPERATIVE ADVICED EXPERT SYSTEMS FOR ONE-SEAT AIRCRAFTS AND STRUCTURE OF THEIR KNOWLEDGE BASES |
ICAS-98-R.6.8 |
Feirertag F. |
CAST AIRFRAME PRIMARY STRUCTURE |
ICAS-98-R.6.1 |
Fergione J. |
TESTING OF AN AUTOMATIC, LOW ALTITUDE, ALL TERRAIN GROUND COLLISION AVOIDANCE SYSTEM |
ICAS-98-1.8.1 |
Ferreres G. |
DESIGN OF FLIGHT CONTROL SYSTEM FOR A HIGHLY FLEXIBLE AIRCRAFT USING CONVEX SYNTHESIS |
ICAS-98-1.5.1 |
Fico G. C. R. |
THREE DIMENSIONAL FLOW SIMULATION IN THE TEST SECTION OF A SLOTTED TRANSONIC WIND TUNNEL |
ICAS-98-R.3.11 |
Fielding J. P. |
SAFETY AND RELIABILITY PREDICTION METHODS FOR AIRCRAFT PRELIMINARY DESIGN |
ICAS-98-6.1.4 |
Filatyev A. S. |
OPTIMIZATION OF SPACE SYSTEM LAUNCHING WITH LIMITATIONS ON FALL ZONES FOR SPENT COMPONENTS |
ICAS-98-1.3.3 |
Fitshugh G. L. |
USING VHDL MODELING AND SIMULATION FOR THE DESIGN OF NEXT-GENERATION WEAPONS SYSTEMS |
ICAS-98-P5 |
Fonarev A. S. |
AERODYNAMIC CHARACTERISTICS OF AXISYMMETRIC AND THREE-DIMENSIONAL BODIES AT TRANSONIC SPEEDS |
ICAS-98-2.4.5 |
Fox J. S. |
INSTANTANEOUS PLIF MEASUREMENT OF SPECIES MOLE-FRACTION IN A VARYING TEMPERATURE SUPERSONIC FLOW |
ICAS-98-3.1.4 |
Frackowiak A. J. |
PREDICTED DEEP-STALL FLIGHT CHARACTERISTICS OF TWO HYPERSONIC FLIGHT VEHICLES |
ICAS-98-1.3.2 |
Frey N. |
FINITE ELEMENT MODELING AND EXPERIMENTAL STUDY OF A GAS TURBINE ENGINE BLADE UNDER BIAXIAL LOADING |
ICAS-98-5.1.4 |
Frulla G. |
EXPERIMENTAL BEHAVIOR OF GRAPHITE / EPOXY PANELS WITH CUT-OUTS UNDER BIAXIAL TENSION, COMPRESSION AND SHEAR LOADS |
ICAS-98-4.4.2 |
Fujita M. |
SELF-EXCITED OSCILLATIONS OF SUPERSONIC OPPOSING JET FLOW |
ICAS-98-2.4.3 |
G. R. |
ESTIMATION OF PILOT MODEL PARAMETERS FOR HELICOPTER HANDLING QUALITIES STUDIES |
ICAS-98-R.6.3 |
Gai S. L. |
BOUNDARY LAYER EFFECTS ON THE BASE PRESSURE BEHIND A BLUNT TRAILING EDGE AEROFOIL |
ICAS-98-3.10.5 |
Gai S. L. |
MIXING DUE TO A SUPERSONIC MAIN STREAM AND CO-FLOWING SUPERSONIC PARALLEL JET |
ICAS-98-3.5.2 |
Gai S. L. |
PLIF IMAGING OF THE SEPARATED REGION BEHIND A CONE IN A HYPERSONIC FLOW |
ICAS-98-3.10.4 |
Galbraith R. A. Mc D. |
A STUDY OF VORTEX BREAKDOWN ON PITCHING DELTA WINGS USING HIGH RESOLUTION PRESSURE MEASUREMENTS |
ICAS-98-3.2.3 |
Galea S. G. |
OPTIMIZATION OF A COMPOSITE BONDED REPAIR TO CRACKED PANELS SUBJECTED TO ACOUSTIC EXCITATION |
ICAS-98-5.3.2 |
Gandolfo A. |
ENGINE SUB-IDLE MODEL |
ICAS-98-5.6.2 |
Gantois K. |
MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMISATION OF AEROSPACE VEHICLES: INCORPORATION OF MANUFACTURING INFORMATION |
ICAS-98-7.2.3 |
Gantois K. |
MULTIDISCIPLINARY DESIGN AND OPTIMISATION OF A LARGE SCALE CIVIL AIRCRAFT WING |
ICAS-98-6.4.2 |
Gardarein P. |
EULER /NAVIER-STOKES SIMULATION FOR PROPULSION-AIRFRAME INTEGRATION OF ADVANCED PROPELLER-DRIVEN AIRCRAFT IN THE EUROPEAN RESEARCH PROGRAMS GEMINI/ APIAN |
ICAS-98-5.10.2 |
Garnier F. |
MODELING EXHAUST JET DILUTION IN AIRCRAFT WAKES: APPLICATION TO THE CONTRAIL FORMATION |
ICAS-98-2.10.1 |
Garry K. P. |
PNEUMATIC YAW CONTROL AT HIGH ANGLE OF ATTACK FOR LOW OBSERVABILITY COMBAT AIRCRAFT |
ICAS-98-1.10.3 |
Garry K. P. |
PREDICTION OF THE VORTICITY FIELD PRODUCED BY AIR-JET VORTEX GENERATORS |
ICAS-98-2.8.2 |
Gear J. A. |
A TIME-MARCHING, TYPE-DEPENDENT, FINITE DIFFERENCE ALGORITHM FOR THE MODIFIED TRANSONIC SMALL DISTURBANCE EQUATION |
ICAS-98-2.6.4 |
Geerling G. |
MORE EFFICIENT FLUID POWER SYSTEMS USING VARIABLE DISPLACEMENT HYDRAULIC MOTORS |
ICAS-98-5.5.1 |
Gia M. C. |
ROUTING ALGORITHMS FOR REAL-TIME MISSION MANAGEMENT |
ICAS-98-6.2.3 |
Gibbens P.W. |
A COMPARISON OF THREE TECHNIQUES FOR THE PREDICTION OF ISOLATED PROPELLER PERFORMANCE |
ICAS-98-5.10.1 |
Gibbs P. |
HMD OFF-BORESIGHT SYMBOLOGY FOR FIXED-WINGS AIRCRAFT: AN EXPERIMENTAL APPROACH |
ICAS-98-6.3.1 |
Gibson A. |
A DESIGN AND TEST PROGRAMME INVOLVING WELDED SHEET-STRINGER COMPRESSION PANELS |
ICAS-98-7.7.3 |
Girardelli E. |
DIAGNOSTIC FROM SYSTEM MODELS: THE ADAM EXPERT SYSTEM APPROACH |
ICAS-98-6.6.2 |
Glinos N. |
THE INFLUENCE OF CORROSION ON THE FATIGUE AND FRACTURE BEHAVIOUR OF 7050-T76 ALUMINIUM ALLOY SPECIMENS CONTAINING COLD EXPANDED HOLES |
ICAS-98-5.2.2 |
Goetzendorf-Grabowski T. |
ANALYSIS OF TRANSIENT DYNAMIC BEHAVIOUR OF A FIRE FIGHTING AIRCRAFT AFTER THE WATER BOMB DROPPING |
ICAS-98-1.4.4 |
Goman M. G. |
WIND TUNNEL SIMULATION OF COMBAT AIRCRAFT MANOEUVRES |
ICAS-98-3.9.2 |
Gorai Z. |
ANALYSIS OF TRANSIENT DYNAMIC BEHAVIOUR OF A FIRE FIGHTING AIRCRAFT AFTER THE WATER BOMB DROPPING |
ICAS-98-1.4.4 |
Goraj Z. |
HIGH ANGLES OF ATTACK FLIGHT DYNAMICS OF CONTEMPORARY AND PROSPECTIVE FIGHTERS AS A FUNCTION OF THEIR CONFIGURATION AND AERODYNAMICS |
ICAS-98-1.7.4 |
Gottero M. |
DPIV ANALYSIS OF WALL TURBULENT SHEAR FLOWS |
ICAS-98-3.1.2 |
Granasy P. |
A SENSITIVITY ANALYSIS OF CHAOS AT HIGH ANGLE OF ATTACK |
ICAS-98-1.7.3 |
Granasy P. |
NONLINEAR CHARACTERISTICS OF TRANSONIC FLUTTER OF A HIGH ASPECT RATIO WING |
ICAS-98-4.1.2 |
Granot Z. |
FATIGUE AND DAMAGE TOLERANCE SUBSTANTIATION OF THE GALAXY EXECUTIVE JET AIRCRAFT |
ICAS-98-5.7.3 |
Grechko I. Y. |
ANALYTICAL AND EXPERIMENTAL INVESTIGATIONS OF AN IMPROVED AERODYNAMIC ORBITER CONFIGURATION |
ICAS-98-R.1.2 |
Green R. B. |
A STUDY OF VORTEX BREAKDOWN ON PITCHING DELTA WINGS USING HIGH RESOLUTION PRESSURE MEASUREMENTS |
ICAS-98-3.2.3 |
Greenwell D. I. |
DIFFICULTIES IN THE APPLICATION OF STABILITY DERIVATIVES TO THE MANOEUVRING AERODYNAMICS OF COMBAT AIRCRAFT |
ICAS-98-1.7. 1 |
Greenwell D. I. |
WIND TUNNEL SIMULATION OF COMBAT AIRCRAFT MANOEUVRES |
ICAS-98-3.9.2 |
Griffin E. |
TESTING OF AN AUTOMATIC, LOW ALTITUDE, ALL TERRAIN GROUND COLLISION AVOIDANCE SYSTEM |
ICAS-98-1.8.1 |
Gronland T. -A. |
ACCURACY OF UNSTEADY TRANSONIC FLOW COMPUTATIONS |
ICAS-98-2.4.2 |
Grubel G. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN PART 3: PHYSICAL MODELING OF AIRCRAFT FOR AUTOMATED LFT GENERATION APPLIED TO THE RESEARCH CIVIL AIRCRAFT MODEL |
ICAS-98-1.6.3 |
Grubel G. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN. PART I : ?-ANALYSIS OF DESIGN ENTRIES TO A ROBUST FLIGHT CONTROL BENCHMARK |
ICAS-98-1.6.1 |
Guerra G. |
LIFE CYCLE COST ESTIMATION TOOL FOR CONCEPTUAL DESIGN |
ICAS-98-6.1.2 |
Guglieri G. |
A STUDY OF SELF INDUCED OSCILLATORY ROLLING MOTION: ANALYTICAL AND EXPERIMENTAL RESULTS |
ICAS-98-1.7.2 |
Guglieri G. |
EFFECT OF MAIN ROTOR CONFIGURATION AND PROPULSION SYSTEM DYNAMICS ON HELICOPTER HANDLING QUALITIES |
ICAS-98-1.4.1 |
Guillaume M. |
SWISS F / A-18 FATIGUE TRACKING SYSTEM |
ICAS-98-5.1.2 |
Guo Y. J. |
PREDICTION OF FATIGUE CRACK GROWTH IN FIBER REINFORCED METAL LAMINATES |
ICAS-98-5.7.5 |
Gupta S. C. |
COMPUTATIONAL ALGORITHMS FOR THE CONFIGURATION DESIGN |
ICAS-98-6.4.5 |
Gurevich B. I. |
RECENT INVESTIGATIONS OF THE VERY LARGE PASSENGER BLENDED-WING-BODY AIRCRAFT |
ICAS-98-4.10.2 |
Habibie I. A |
N2130: A NEW REGIONAL AIRLINER FOR THE 21 ST CENTURY |
ICAS-98-4.10.4 |
Hackett K. C. |
AERODYNAMIC DESIGN OPTIMISATION APPLIED TO CIVIL TRANSPORTS WITH UNDERWING MOUNTED ENGINES |
ICAS-98-2.3.1 |
Hackett K. C. |
AERODYNAMIC SCALE EFFECTS ON A TRANSPORT-AIRCRAFT MODEL AT HIGH SUBSONIC SPEED |
ICAS-98-P6 |
Hagelauer P. |
A SOFT DYNAMIC PROGRAMMING APPROACH FOR ON-LINE AIRCRAFT 4D-TRAJECTORY OPTIMIZATION |
ICAS-98-6.2.1 |
Hah C. |
DEVELOPMENT OF ENDWALL FLOW AND TIP-CLEARANCE VORTEX IN AN AXIAL PUMP STAGE |
ICAS-98-5.4.2 |
Hamner O. |
AERODYNAMIC CHARACTERISTICS OF MISSILES WITH TRIANGULAR CROSS SECTIONS |
ICAS-98-3.6.3 |
Han S. |
SUPERSONIC UNDEREXPANDED RECTANGULAR JET OSCILLATIONS: A COMPUTATIONAL STUDY |
ICAS-98-2.10.5 |
Hanff E. S. |
FLOW PHYSICS OF LEADING-EDGE VORTEX-BREAKDOWN |
ICAS-98-3.2.1 |
Hannemann M. |
MANUAL AERODYNAMIC OPTIMIZATION OF OBLIQUE FLYING WING |
ICAS-98-2.1.3 |
Hart-Smith L. J. |
ON THE ADVERSE CONSEQUENCES OF COST-PERFORMANCE METRICS USURPING THE ROLE OF GOALS THEY WERE SUPPOSED TO SUPPORT |
ICAS-98-6.1.1 |
Hasegawa H. |
THE MECHANISM OF ACTIVE BOUNDARY LAYER CONTROL USING VORTEX GENERATOR JETS |
ICAS-98-3.4.3 |
Haselbach F. |
CAPABILITIES OF SURFACE MEASUREMENT TECHNIQUES AND THEIR IMPACT ON MODERN WING-DESIGN AND ASSESSMENT |
ICAS-98-3.3.4 |
Haverdings H. |
EVALUATION OF WINDSHEAR HAZARD DISPLAYS AND GO-AROUND PROCEDURES USING PILOTED SIMULATIONS AT NLR |
ICAS-98-6.7.2 |
Hazarika N. |
AN INVERSE DESIGN PROCEDURE FOR AIRFOILS USING ARTIFICIAL NEURAL NETWORKS |
ICAS-98-2.2.1 |
Hedo J. M. |
STRATEGIES FOR MINIMUM DISTANCE IN SIMULATED EVACUATION OF TRANSPORT AIRPLANES |
ICAS-98-6.7.5 |
Hegde U. |
CHARACTERISTICS OF MOMENTUM-DOMINATED HYDROCARBON TURBULENT DIFFUSION FLAMES |
ICAS-98-5.8.1 |
Hegedus M. C. |
PREDICTED DEEP-STALL FLIGHT CHARACTERISTICS OF TWO HYPERSONIC FLIGHT VEHICLES |
ICAS-98-1.3.2 |
Hegedus M. C. |
PREDICTION OF HIGH-? AERODYNAMIC CHARACTERISTICS OF MANEUVERING AIRCRAFT |
ICAS-98-1.7.5 |
Heller M. |
INVESTIGATION OF SHAPE OPTIMISATION TECHNIQUES FOR THE DESIGN OF PLATES WITH CUT-OUTS |
ICAS-98-4.7.5 |
Henke R. |
THE AIRBUS A320 HYBRID LAMINAR FLOW FIN PROGRAMME |
ICAS-98-3.4.1 (Invited paper) |
Hernandez C. |
STRATEGIES FOR MINIMUM DISTANCE IN SIMULATED EVACUATION OF TRANSPORT AIRPLANES |
ICAS-98-6.7.5 |
Herszberg I. |
COMPRESSIONS AFTER IMPACT BEHAVIOUR OF MULTILAYER WOVEN GLASS/VINYL ESTER COMPOSITES |
ICAS-98-5.9.1 |
Herszberg I. |
CONTROL OF HIGH ENDURANCE UNMANNED AIR VEHICLE |
ICAS-98-3.7.1 |
Heyma P. M. |
A SIMPLE WING OPTIMISATION CODE INCLUDING PROPELLER EFFECTS |
ICAS-98-2.3.4 |
Heywood M. |
IMPROVING THE AERODYNAMIC EFFICIENCY OF A WING BY ACOUSTIC EXCITATION |
ICAS-98-3.9.4 |
Hierholz K. -H. |
SIMULATION OF FLUID-STRUCTURE INTERACTION AT THE HELICOPTER ROTOR |
ICAS-98-2.5.1 |
Hodges D. H. |
NONLINEAR AEROELASTICITY AND FLIGHT DYNAMICS OF AIRCRAFT IN SUBSONIC FLOW |
ICAS-98-7.7.4 |
Hoeijmakers H. W. M. |
COMPUTATIONAL UNSTEADY AERODYNAMICS IN AEROELASTIC SIMULATION |
ICAS-98-4.6.3 |
Hoeijmakers H. W. M. |
NUMERICAL SIMULATION OF THE UNSTEADY AERODYNAMIC RESPONSE OF A COMPLETE AIRCRAFT |
ICAS-98-2.4.1 |
Hoekstra J. M. |
COCKPIT SYSTEMS REQUIREMENTS IN A FUTURE ATM ENVIRONMENT |
ICAS-98-6.2.2 |
Hoffren J. |
CALIBRATION OF AIR COMBAT SIMULATION MODELS BASED ON PERFORMANCE DATA |
ICAS-98-2.11.2 |
Holding J. P. |
DEVELOPMENT OF THE GLOBAL EXPRESS: A SUCCESS OF INTERNATIONAL PARTNERSHIP |
ICAS-98-0.5 (Von Karman Lecture) |
Hong G. |
A MATHEMATICAL MODEL OF AFFINE NONLINEAR SYSTEM FOR HELICOPTER FLIGHT DYNAMICS |
ICAS-98-1.4.5 |
Houniet M. H. L. |
COMPREHENSIVE TIME ANALYSIS IN AEROELASTIC SIMULATIONS |
ICAS-98-4.3.3 |
Hounjet M. H. L. |
COMPUTATIONAL UNSTEADY AERODYNAMICS IN AEROELASTIC SIMULATION |
ICAS-98-4.6.3 |
Hounjet M. H. L. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Houwing A. F. P. |
INSTANTANEOUS PLIF MEASUREMENT OF SPECIES MOLE-FRACTION IN A VARYING TEMPERATURE SUPERSONIC FLOW |
ICAS-98-3.1.4 |
Houwing A. F. P. |
PLIF IMAGING OF THE SEPARATED REGION BEHIND A CONE IN A HYPERSONIC FLOW |
ICAS-98-3.10.4 |
Huang A. |
AIRCRAFT LOAD MODELS FOR A PILATUS PC-9 BASED ON WIND TUNNEL TESTING |
ICAS-98-7.6.1 |
Huang X. L. |
FLOW PHYSICS OF LEADING-EDGE VORTEX-BREAKDOWN |
ICAS-98-3.2.1 |
Huffman R. |
APPLICATION OF GROUND COLLISION AVOIDANCE SYSTEM NUISANCE CRITERIA |
ICAS-98-1.8.3 |
Hulshoff S. J. |
NUMERICAL SIMULATION OF THE UNSTEADY AERODYNAMIC RESPONSE OF A COMPLETE AIRCRAFT |
ICAS-98-2.4.1 |
Hummel D. |
EXPERIMENTAL AND NUMERICAL INVESTIGATIONS ON WAVERIDERS IN DIFFERENT FLIGHT REGIMES |
ICAS-98-2.1.4 |
Hummel D. |
LOW SPEED WIND TUNNEL EXPERIMENTS ON A DELTA WING OSCILLATING IN PITCH |
ICAS-98-3.9.3 |
Indrawanto |
N-2S0 PROTOTYPE 1 FLIGHT FLUTTER TESTING DEVELOPMENT |
ICAS-98-4.5.3 |
Innocenti M. |
EVALUATION OF VARIABLE STRUCTURE METHODS FOR AUTOPILOT DESIGN OF AGILE MISSILES |
ICAS-98-1.6.4 |
Innocenti M. |
NONLINEAR PILOT IN THE LOOP PERFORMANCE USING A MODIFIED CROSSOVER MODEL |
ICAS-98-6.3.2 |
Ishmuratov F. |
THEORETICAL STUDY OF TRANSONIC FLUTTER/BUZZ IN THE FREQUENCY AND TIME DOMAIN |
ICAS-98-4.9.2 |
Isikveren A. T. |
METHODOLOGY FOR CONCEPTUAL DESIGN AND OPTIMISATION OF TRANSPORT AIRCRAFT |
ICAS-98-7.2.2 |
Ithurralde C. |
AN IMPROVED FATIGUE APPROACH FOR DESIGNING AIRCRAFT JOINTS |
ICAS-98-5.3.4 |
Jacob K. A. |
PROBABILISTIC APPROACH FOR DESIGN OF A COMPOSITE RPV WING |
ICAS-98-R.4.7 |
Jacob K. A. |
PROBABILISTIC APPROACH FOR DESIGN OF A COMPOSITE RPVWING. |
ICAS-98-5.9.4 |
Jancelewicz B. |
SOME INVESTIGATIONS ON WOOD-COMPOSITE STRUCTURES FOR VERY LIGHT AIRCRAFT (VLA) |
ICAS-98-4.4.4 |
Jankovic J. |
COMPUTER VISUALISATION AND SIMULATION OF FAST CYCLIC HYDRAULIC ACTUATOR DYNAMICS |
ICAS-98-5.5.3 |
Jazwinski J. |
APPLICATION OF EXPERT METHODS TO RISK ASSESSMENT OF AIR TRANSPORT SYSTEMS |
ICAS-98-R.1.9.2 |
Jenkinson L. R. |
DEVELOPMENT OF AN INTEGRATED CONCEPTUAL AIRCRAFT DESIGN AND AIRCRAFT NOISE MODEL FOR CIVIL TRANSPORT AIRCRAFT |
ICAS-98-6.4.3 |
Jenkinson L. R. |
ESTIMATION OF CIVIL AIRCRAFT PERFORMANCE AND OPERATING PRACTICES FROM RADAR DATA |
ICAS-98-5.11.1 |
Jeremic S. |
RELIABILITY EVALUATION OF AEROSPACE COMPONENTS |
ICAS-98-7.1.3 |
Jeremic S. |
THREE DIMENSIONAL ROTOR FLOW CALCULATION |
ICAS-98-7.4.5 |
Jin J. |
RESEARCH OF ACTIVE VIBRATION CONTROL TECHNOLOGIES FOR A COMPOSITE SHELL |
ICAS-98-4.11.1 |
Jonsson B. |
AERODYNAMIC CHARACTERISTICS OF MISSILES WITH TRIANGULAR CROSS SECTIONS |
ICAS-98-3.6.3 |
Jou W. H. |
A SYSTEMS APPROACH TO CFD CODE DEVELOPMENT |
ICAS-98-2.7.5 |
Journet B. |
AN IMPROVED FATIGUE APPROACH FOR DESIGNING AIRCRAFT JOINTS |
ICAS-98-5.3.4 |
Jupp M. L. |
A STUDY OF VORTEX BREAKDOWN ON PITCHING DELTA WINGS USING HIGH RESOLUTION PRESSURE MEASUREMENTS |
ICAS-98-3.2.3 |
Kadar M. |
A NUMERICAL STUDY OF LIFTING SURFACE AEROELASTIC INSTABILITY USING TRANSONIC UNSTEADY AERODYNAMIC CODE -NTRANS |
ICAS-98-4.6.2 |
Kanagarajan V. |
UNSTEADY TRANSONIC HYBRID INTEGRAL-EQUATION / FINITE-VOLUME SCHEME FOR TRAJECTORY SIMULATION OF STORES WITH TIME-STEP ADAPTATION |
ICAS-98-2.4.4 |
Karashima K. |
SELF-EXCITED OSCILLATIONS OF SUPERSONIC OPPOSING JET FLOW |
ICAS-98-2.4.3 |
Karpel M. |
STRUCTURAL OPTIMIZATION WITH STATIC CONSTRAINTS USING EXPANDABLE MODAL BASIS |
ICAS-98-4.7.2 |
Kehayas N. |
THE BLENDED WING-BODY CONFIGURATION AS AN ALTERNATIVE TO CONVENTIONAL SUBSONIC CIVIL TRANSPORT AIRCRAFT DESIGN |
ICAS-98-4.10.5 |
Kim I. |
USE OF CFD FOR DESIGN VALIDATION OF A TRANSONIC CIVIL TRANSPORT |
ICAS-98-2.3.3 |
Kirekland L. |
THE RISKS OF OVERRUNS |
ICAS-98-1.11.1 |
Kiselev A. P. |
EXPERIMENTAL INVESTIGATION ON THE APPLICATION OF HYBRID LAMINAR FLOW CONTROL TO LARGE-SCALE SWEPT WING MODELS AT SUBSONIC SPEEDS |
ICAS-98-3.4.2 |
Klukowski K. |
APPLICATION OF A FLIGHT SIMULATOR FOR SELECTION OF PILOT-CANDIDATES |
ICAS-98-6.3.3 |
Kneen J |
A TOOLSET FOR THE DESIGN OF AUTONOMOUS UAV SYSTEMS |
ICAS-98-3.7.3 |
Knowles K. |
SENSITIVITY OF STOVL AIRCRAFT AERODYNAMICS TO INTAKE MODELLING |
ICAS-98-P7 |
Kokkalis A. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Kolonay R. |
CONTROL SURFACE EFFECTIVENESS IN THE TRANSONIC REGIME |
ICAS-98-4.6.4 |
Kopadoulos G. G. |
AIRCRAFT LANDING-A TOTAL SYSTEM APPROACH |
ICAS-98-1.11.2 |
Korzenowski H. |
ADAPTIVE MESH REFINEMENT ON THE SOLUTION OF TWO-DIMENSIONAL VISCOUS AEROSPACE PROBLEMS |
ICAS-98-2.2.3 |
Kossowski J. |
APPLICATION OF A FLIGHT SIMULATOR FOR SELECTION OF PILOT-CANDIDATES |
ICAS-98-6.3.3 |
Kostic I. |
AN IMPROVED METHOD FOR THE DESIGN AND CALCULATION OF AERODYNAMIC CHARACTERISTICS OF AIRFOILS WITH THE DOMINANT TURBULENT BOUNDARY LAYER AT SUBSONIC AND LOWER TRANSONIC SPEEDS |
ICAS-98-2.9.3 |
Kouzmina S. |
THEORETICAL STUDY OF TRANSONIC FLUTTER/BUZZ IN THE FREQUENCY AND TIME DOMAIN |
ICAS-98-4.9.2 |
Kranz O. |
FLYING OBJECTS - AN OBJECT-ORIENTED TOOLBOX FOR MULTIDISCIPLINARY DESIGN AND EVALUATION OF AIRCRAFT |
ICAS-98-6.4.4 |
Kravchenko I. V. |
EXPERIMENTAL INVESTIGATION OF WORKING PROCESS OF THE FRONT DEVICES WITH OPPOSITE FLOW TWISTING, WHICH ARE USED IN THE COMBUSTION CHAMBERS WITH REFINED ECOLOGICAL PERFORMANCES |
ICAS-98-5.8.3 |
Kreiselmaier E. |
SMALL DISTURBANCE EULER EQUATIONS (SDEE) -AN EFFICIENT AND ACCURATE TOOL FOR UNSTEADY LOAD PREDICTIONS AT ALL MACH NUMBERS |
ICAS-98-2.6.3 |
Krol R. J. |
FROM A MONO-DISCIPLINARY TO A MULTI-DISCIPLINARY APPROACH IN AEROSPACE: AS SEEN FROM AN INFORMATION AND COMMUNICATION TECHNOLOGY PERSPECTIVE |
ICAS-98-6.8.2 |
Kroll N. |
MEGAFLOW -A NUMERICAL FLOW SIMULATION SYSTEM |
ICAS-98-2.7.4 |
Kroll N. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Kubica F. |
FLEXIBLE STRUCTURE CONTROL BY MODAL MULTI-MODEL APPROACH: APPLIED TO FLEXIBLE AIRCRAFT |
ICAS-98-1.5.2 |
Kubica F. |
NEW FLIGHT CONTROL LAWS FOR LARGE CAPACITY AIRCRAFT EXPERIMENTATION ON AIRBUS A340 |
ICAS-98-1.5.3 |
Kubrynski K. |
AERODYNAMIC DESIGN OF HIGH-PERFORMANCE SAILPLANE WING-FUSELAGE COMBINATIONS |
ICAS-98-2.9.2 |
Kundu A. K. |
A PROPOSITION IN DESIGN EDUCATION WITH A POTENTIAL IN COMMERCIAL VENTURE IN SMALL AIRCRAFT MANUFACTURE |
ICAS-98-6.4.1 |
Kuntjoro W. |
AIRFRAME CONFIGURATION DESIGN USING CONSTRAINT PROPAGATION TECHNIQUE CASE WING STRUCTURE |
ICAS-98-4.2.3 |
La Roche U. |
DEVELOPMENT, QUALIFICATION AND FLIGHT TESTING OF A WINGGRID ON A JET-POWERED TESTBED |
ICAS-98-1.1.4 |
La Roche U. |
OBLIQUE GROOVES AVOIDING LAMINAR FLOW SEPARATION ON BODIES IN POSITIVE PRESSURE GRADIENTS |
ICAS-98-3.4.4 |
Laban M. |
FROM A MONO-DISCIPLINARY TO A MULTI-DISCIPLINARY APPROACH IN AEROSPACE: AS SEEN FROM AN INFORMATION AND COMMUNICATION TECHNOLOGY PERSPECTIVE |
ICAS-98-6.8.2 |
Lai J. C. S. |
APPLICATION OF AN IMPROVED KˇE MODEL TO SEPARATION FLOWS |
ICAS-98-3.10.1 |
Lai J. C. S. |
REATTACHMENT OF AN INCLINED WALL JET |
ICAS-98-3.5.1 |
Lambrianidis L. T. |
BOND DURABILITY PERFORMANCE -THE AUSTRALIAN SILANE SURFACE TREATMENT |
ICAS-98-5.3.1 |
Langlois M. |
STABILITY ANALYSIS BY THE OS AND PSE APPROACHES: COMPARISONS WITH EXPERIMENTS |
ICAS-98-2.8.1 |
Laschka B. |
SMALL DISTURBANCE EULER EQUATIONS (SDEE) -AN EFFICIENT AND ACCURATE TOOL FOR UNSTEADY LOAD PREDICTIONS AT ALL MACH NUMBERS |
ICAS-98-2.6.3 |
Laschka B. |
VORTICAL FLOWFIELD STRUCTURE AT FORWARD SWEPT WING CONFIGURATIONS |
ICAS-98-3.8.2 |
Laverdant A. |
MODELING EXHAUST JET DILUTION IN AIRCRAFT WAKES: APPLICATION TO THE CONTRAIL FORMATION |
ICAS-98-2.10.1 |
Le Gorrec Y. |
FLEXIBLE STRUCTURE CONTROL BY MODAL MULTI-MODEL APPROACH: APPLIED TO FLEXIBLE AIRCRAFT |
ICAS-98-1.5.2 |
Le Pimpec M. |
ULTRASONIC TECHNOLOGY: A SOLUTION FOR IN-FLIGHT AND ON-GROUND ICE DETECTION |
ICAS-98-6.7.1 |
Leacock |
ESTIMATION OF PILOT MODEL PARAMETERS FOR HELICOPTER HANDLING QUALITIES STUDIES |
ICAS-98-R.6.3 |
Lee C. A. |
THE SENSITIVITY OF SCT DESIGNS TO AIRFIELD NOISE REQUIREMENTS: AN INVESTIGATION USING MULTIVARIATE OPTIMISATION |
ICAS-98-1.2.1 |
Lee K. D. |
TURBOMACHINERY BLADE DESIGN USING THE NAVIER-STOKES EQUATIONS |
ICAS-98-5.4.4 |
Lee Y. |
DEVELOPMENT OF ENDWALL FLOW AND TIP-CLEARANCE VORTEX IN AN AXIAL PUMP STAGE |
ICAS-98-5.4.2 |
Leger A. |
HMD OFF-BORESIGHT SYMBOLOGY FOR FIXED-WINGS AIRCRAFT: AN EXPERIMENTAL APPROACH |
ICAS-98-6.3.1 |
Lemee P. |
ONERA ACTIVITIES ON SUPERSONIC TRANSPORT AIRCRAFT AERODYNAMICS |
ICAS-98-2.1.2 |
Leppert F. |
HMD OFF-BORESIGHT SYMBOLOGY FOR FIXED-WINGS AIRCRAFT: AN EXPERIMENTAL APPROACH |
ICAS-98-6.3.1 |
Lewitowicz J. |
DETERMINATION OF FLIGHT-SAFETY RATES AND EXAMINATION OF THEIR VARIATIONS WITH TIME IN CORRELATION TO RELIABILITY RATES |
ICAS-98-6.7.4 |
Lewitowicz J. |
THE NEURAL DIAGNOSTIC METHOD AND A COMPLEX SYSTEM OF DIAGNOSING AIRFRAME AND POWERPLANT |
ICAS-98-6.6.4 |
Li J. |
LOAD TRANSFER MECHANISM IN BOLTED DOUBLE LAP JOINTS |
ICAS-98-5.3.3 |
Li P. |
MANUAL AERODYNAMIC OPTIMIZATION OF OBLIQUE FLYING WING |
ICAS-98-2.1.3 |
Li W. J. |
THE METHOD FOR COMPUTING THE FAILURE PROBABILITY OF AIRCRAFT STRUCTURES |
ICAS-98-R.5.7 |
Li X. |
A NEW, AVAILABLE HIGH-PRECISION CCD ANGLE-MEASURING SENSOR IN AERONAUTICS AND ASTRONAUTICS |
ICAS-98-R.5.11 |
Li Yuan |
EFFECTS OF USING BI-FLAP-SYSTEM ON THE IMPROVEMENT OF AERODYNAMICS OF A SWEPTBACK WING |
ICAS-98-3.6.2 |
Li Z. |
STUDY OF WING STRUCTURAL LAYOUT DECISION SUPPORT SYSTEM |
ICAS-98-4.7.4 |
Lind R. |
ON - LINE ROBUST MODAL STABILILY PREDICTION USING WAVELET PROCESSING |
ICAS-98-4.9.1 |
Lindblad I. |
PROPELLER SLIPSTREAM COMPUTATIONAL METHODS |
ICAS-98-2.6.2 |
Lindstedt P. |
THE NEURAL DIAGNOSTIC METHOD AND A COMPLEX SYSTEM OF DIAGNOSING AIRFRAME AND POWERPLANT |
ICAS-98-6.6.4 |
Link Y. Y. |
TRANSONIC WIND TUNNEL OT THE AERONOUTICAL AND MARITIME RESEARCH LABORATORY |
ICAS-98-P8 |
Liu G. |
RESEARCH OF ACTIVE VIBRATION CONTROL TECHNOLOGIES FOR A COMPOSITE SHELL |
ICAS-98-4.11.1 |
Liu J. |
A NEW, AVAILABLE HIGH-PRECISION CCD ANGLE-MEASURING SENSOR IN AERONAUTICS AND ASTRONAUTICS |
ICAS-98-R.5.11 |
Llanes L. |
THE EVOLUTION UNDER STRESS OF THE SUPERALLOY / PROTECTIVE COATING INTERFACE |
ICAS-98-4.2.2 |
Loellbach J. |
DEVELOPMENT OF ENDWALL FLOW AND TIP-CLEARANCE VORTEX IN AN AXIAL PUMP STAGE |
ICAS-98-5.4.2 |
Loeser T. |
LOW SPEED WIND TUNNEL EXPERIMENTS ON A DELTA WING OSCILLATING IN PITCH |
ICAS-98-3.9.3 |
Lombardi G. |
VORTICITY MEASUREMENTS IN THE NEAR-FIELD OF A WING TIP VORTEX |
ICAS-98-3.2.2 |
Long G. |
FUTURE DIRECTIONS IN AERONAUTICAL COMPOSITES |
ICAS-98-0.1 (Daniel and Florence Guggenheim Memorial Lecture) |
Looye G. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN PART 3: PHYSICAL MODELING OF AIRCRAFT FOR AUTOMATED LFT GENERATION APPLIED TO THE RESEARCH CIVIL AIRCRAFT MODEL |
ICAS-98-1.6.3 |
Looye G. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN. PART I : ?-ANALYSIS OF DESIGN ENTRIES TO A ROBUST FLIGHT CONTROL BENCHMARK |
ICAS-98-1.6.1 |
Looye G. Bennani S. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN PART 2: EVALUATION OF A NEW TOOL FOR ?-ANALYSIS |
ICAS-98-1.6.2 |
Lovell D. A. |
REDUCTION OF WAVE AND LIFT-DEPENDENT DRAG FOR SUPERSONIC TRANSPORT AIRCRAFT |
ICAS-98-2.1.1 |
Lovgren J. |
RESULTS OF A JOINT US/SWEDISH AUTO GROUND COLLISION AVOIDANCE SYSTEM PROGRAM |
ICAS-98-1.8.2 |
Lowe D. |
AN INVERSE DESIGN PROCEDURE FOR AIRFOILS USING ARTIFICIAL NEURAL NETWORKS |
ICAS-98-2.2.1 |
Lu D. |
REATTACHMENT OF AN INCLINED WALL JET |
ICAS-98-3.5.1 |
Lu Z. Z. |
THE METHOD FOR COMPUTING THE FAILURE PROBABILITY OF AIRCRAFT STRUCTURES |
ICAS-98-R.5.7 |
Lucht R. R. |
BRAZILIAN F-S EXTERNAL STORES AEROELASTIC INTEGRATION |
ICAS-98-4.5.2 |
luso G. |
SKIN FRICTION MEASUREMENTS DOWNSTREAM OF A BACK-FACING STEP |
ICAS-98-3.10.3 |
Lutton M. |
ACFD APPLICATIONS TO STORE SEPARATION |
ICAS-98-2.10.4 |
Lutz T. |
NUMERICAL SHAPE OPTIMIZATION OF NATURAL LAMINAR FLOW BODIES |
ICAS-98-2.9.4 |
Ly E. |
A TIME-MARCHING, TYPE-DEPENDENT, FINITE DIFFERENCE ALGORITHM FOR THE MODIFIED TRANSONIC SMALL DISTURBANCE EQUATION |
ICAS-98-2.6.4 |
Ly E. |
IMPROVED APPROXIMATE FACTORISATION ALGORITHM FOR THE STEADY SUBSONIC AND TRANSONIC FLOW OVER AN AIRCRAFT WING |
ICAS-98-7.4.1 |
Lynch C. J. |
A FINITE ELEMENT STUDY OF THE POST-BUCKLING BEHAVIOUR OF A FLAT STIFFENED PANEL |
ICAS-98-7.7.2 |
Ma D. M. |
FLY SIMULATION WITH PERSONNAL COMPUTER NETWORK |
ICAS-98-P9 |
MacCormack R. W. |
A FAST AND ACCURATE METHOD FOR SOLVING THE NAVIER-STOKES EQUATIONS |
ICAS-98-2.7.2 |
MacDonald P. |
STABILITY ANALYSIS BY THE OS AND PSE APPROACHES: COMPARISONS WITH EXPERIMENTS |
ICAS-98-2.8.1 |
Maciel E. S. G. |
ADAPTIVE MESH REFINEMENT ON THE SOLUTION OF TWO-DIMENSIONAL VISCOUS AEROSPACE PROBLEMS |
ICAS-98-2.2.3 |
Magni J. -F. |
FLEXIBLE STRUCTURE CONTROL BY MODAL MULTI-MODEL APPROACH: APPLIED TO FLEXIBLE AIRCRAFT |
ICAS-98-1.5.2 |
Magni J. -F. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN PART 2: EVALUATION OF A NEW TOOL FOR ?-ANALYSIS |
ICAS-98-1.6.2 |
Maler Z. |
THE DAMAGE LIFE OF THE SMALL DIAMETER STEEL CABLES AND THEIR RESIDUAL STATIC STRENGTH |
ICAS-98-P10 |
Mangalam S. |
IN-FLIGHT SHOCK DETECTION USING HOT FILM SENSORS AND CONSTANT VOLTAGE ANEMOMETER SYSTEM |
ICAS-98-3.3.3 |
Marchetti M. |
NUMERICAL SIMULATION OF FLUID-STRUCTURE INTERACTION IN AIRCRAFT FUEL TANKS SUBJECTED TO HYDRODYNAMIC RAM PENETRATION |
ICAS-98-4.3.1 |
Marchetto A. |
ALLOCATION OF FAULT HANDLING TECHNIQUES IN MULTIPROCESSING AVIONICS ARCHITECTURES |
ICAS-98-1.9.2 |
Maresca Ch. |
3D BOUNDARY-LAYER ON ROTATING WINGS: EXPERIMENTS AND CALCULATIONS |
ICAS-98-3.1.1 |
Marques F. D. |
IDENTIFICATION OF AIRCRAFT NON-LINEAR DYNAMICS USING VOLTERRA SERIES |
ICAS-98-1.10.5 |
Martinez-Val R. |
STRATEGIES FOR MINIMUM DISTANCE IN SIMULATED EVACUATION OF TRANSPORT AIRPLANES |
ICAS-98-6.7.5 |
Martins A. L. |
VISCOUS DRAG OPTIMIZATION FOR A TRANSPORT AIRCRAFT MISSION ADAPTIVE WING |
ICAS-98-2.3.2 |
Marulo F. |
NUMERICAL, WIND-TUNNEL AND FLIGHT TESTS FOR P92J AND P96 LIGHT AIRCRAFT |
ICAS-98-3.11.2 |
Masson C. |
STABILITY ANALYSIS BY THE OS AND PSE APPROACHES: COMPARISONS WITH EXPERIMENTS |
ICAS-98-2.8.1 |
Matraia A. |
EVALUATION OF VARIABLE STRUCTURE METHODS FOR AUTOPILOT DESIGN OF AGILE MISSILES |
ICAS-98-1.6.4 |
Matsushita H. |
NONLINEAR CHARACTERISTICS OF TRANSONIC FLUTTER OF A HIGH ASPECT RATIO WING |
ICAS-98-4.1.2 |
Matsuuchi K. |
THE MECHANISM OF ACTIVE BOUNDARY LAYER CONTROL USING VORTEX GENERATOR JETS |
ICAS-98-3.4.3 |
Mavris D. N. |
A STOCHASTIC DESIGN APPROACH FOR AIRCRAFT AFFORDABILITY |
ICAS-98-6.1.3 |
Mayrhofer M. |
OPTIMAL THREE-DIMENSIONAL RANGE CRUISE OF A DUAL-FUEL HYPERSONIC VEHICLE |
ICAS-98-1.3.1 |
Mazurek K. |
APPLICATION OF A FLIGHT SIMULATOR FOR SELECTION OF PILOT-CANDIDATES |
ICAS-98-6.3.3 |
McKenzie G. J. |
AN ENGINEERING METHODOLOGY FOR SUBSONIC STORE TRAJECTORY PREDICTION |
ICAS-98-2.10.3 |
Meehan J. |
HMD OFF-BORESIGHT SYMBOLOGY FOR FIXED-WINGS AIRCRAFT: AN EXPERIMENTAL APPROACH |
ICAS-98-6.3.1 |
Meijer S. |
PROPELLER SLIPSTREAM COMPUTATIONAL METHODS |
ICAS-98-2.6.2 |
Mello O. A. F. |
SIMULATION OF HELICOPTER FLIGHT DYNAMICS AFTER TAIL ROTOR LOSS OR MAIN ROTOR BLADE FAILURE |
ICAS-98-4.1.3 |
Mendenhall M. R. |
PREDICTED DEEP-STALL FLIGHT CHARACTERISTICS OF TWO HYPERSONIC FLIGHT VEHICLES |
ICAS-98-1.3.2 |
Mendenhall M. R. |
PREDICTION OF HIGH-? AERODYNAMIC CHARACTERISTICS OF MANEUVERING AIRCRAFT |
ICAS-98-1.7.5 |
MeyerˇPiening H. R. |
DEVELOPMENT, QUALIFICATION AND FLIGHT TESTING OF A WINGGRID ON A JET-POWERED TESTBED |
ICAS-98-1.1.4 |
Mikeladze V. G. |
EXPERIMENTAL INVESTIGATION ON THE APPLICATION OF HYBRID LAMINAR FLOW CONTROL TO LARGE-SCALE SWEPT WING MODELS AT SUBSONIC SPEEDS |
ICAS-98-3.4.2 |
Milthorpe J. |
APPLICATION OF AN IMPROVED KˇE MODEL TO SEPARATION FLOWS |
ICAS-98-3.10.1 |
Mirsafian S. |
PREDICTION OF ANTISYMMETRIC BUFFET LOADS ON HORIZONTAL STABILIZERS IN MASSIVELY SEPARATED FLOWS |
ICAS-98-4.1.1 |
Mitrovic C. |
OPTIMAL MAIN HELICOPTER ROTOR PROJECTION MODEL OBTAINED BY VISCOUS EFFECTS AND UNSTEADY LIFT SIMULATION |
ICAS-98-2.5.3 |
Miyazawa Y. |
FLIGHT TESTING OF ALFLEX GUIDANCE, NAVIGATION AND CONTROL SYSTEM |
ICAS-98-1.1.3 |
Moes T. M. |
IN-FLIGHT SHOCK DETECTION USING HOT FILM SENSORS AND CONSTANT VOLTAGE ANEMOMETER SYSTEM |
ICAS-98-3.3.3 |
Mohan S. R. |
UNSTEADY TRANSONIC HYBRID INTEGRAL-EQUATION / FINITE-VOLUME SCHEME FOR TRAJECTORY SIMULATION OF STORES WITH TIME-STEP ADAPTATION |
ICAS-98-2.4.4 |
Moir S. A. |
A FLOW VISUALISATION STUDY OF THE DYNAMIC STALLING OF TWO WING PLANFORMS |
ICAS-98-7.3.3 |
Molent L. |
A UNIFIED APPROACH TO FATIGUE USAGE MONITORING OF FIGHTER AIRCRAFT BASED ON F/A-18 EXPERIENCE |
ICAS-98-5.1.3 |
Montel B. |
MULTI-OBJECTIVE STRATEGIES FOR COMPLEX OPTIMIZATION PROBLEMS IN AERODYNAMICS USING GENETIC ALGORITHMS |
ICAS-98-2.9.1 |
Moormann D. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN PART 3: PHYSICAL MODELING OF AIRCRAFT FOR AUTOMATED LFT GENERATION APPLIED TO THE RESEARCH CIVIL AIRCRAFT MODEL |
ICAS-98-1.6.3 |
Moormann D. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN. PART I : ?-ANALYSIS OF DESIGN ENTRIES TO A ROBUST FLIGHT CONTROL BENCHMARK |
ICAS-98-1.6.1 |
Morino L. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Morishita E. |
CONICAL EULER EQUATIONS' SOLUTION BASED ON THE UNSTRUCTURED GRID AND ITS APPLICATION TO A VORTICAL FLOW OVER A HIGHLY SWEPT DELTA WING |
ICAS-98-7.4.2 |
Mornand X. |
CONCEPTUAL DESIGN OF A VERTICAL SITUATION INDICATOR |
ICAS-98-7.1.2 |
Morris A. J. |
MULTIDISCIPLINARY DESIGN AND OPTIMISATION OF A LARGE SCALE CIVIL AIRCRAFT WING |
ICAS-98-6.4.2 |
Morris C. |
PERFORMANCE FLIGHT TESTING OF AN F-111 C AIRCRAFT |
ICAS-98-1.1.1 |
Morris C. E. M. |
BOND DURABILITY PERFORMANCE -THE AUSTRALIAN SILANE SURFACE TREATMENT |
ICAS-98-5.3.1 |
Mosounov V. |
THEORETICAL STUDY OF TRANSONIC FLUTTER/BUZZ IN THE FREQUENCY AND TIME DOMAIN |
ICAS-98-4.9.2 |
Moss J. N. |
MARS ENTRY VEHICLE AERODYNAMIC FLIGHT MEASUREMENTS |
ICAS-98-1.2.3 |
Moulin B. |
STRUCTURAL OPTIMIZATION WITH STATIC CONSTRAINTS USING EXPANDABLE MODAL BASIS |
ICAS-98-4.7.2 |
Mouser C. |
DYNAMIC LOAD DEVELOPMENT AND RESULTS FOR DYNAMIC EXCITATION OF A FULL-SCALE F/A-18 FATIGUE TEST ARTICLE |
ICAS-98-4.5.1 |
Mudford N. |
APPLICATION OF AN IMPROVED KˇE MODEL TO SEPARATION FLOWS |
ICAS-98-3.10.1 |
Mudford N. R. |
PLIF IMAGING OF THE SEPARATED REGION BEHIND A CONE IN A HYPERSONIC FLOW |
ICAS-98-3.10.4 |
Mukhraiya J. K. |
EXPERIMENTAL INVESTIGATION OF AXIAL COMPRESSOR CASCADE PERFORMANCE UNDER THE INFLUENCE OF LOW INTENSITY TURBULENCE |
ICAS-98-5.4.5 |
Munro C. |
FLOW VISUALISATION OF A THRUST VECTORING STOL FIGHTER CONFIGURATION |
ICAS-98-7.3.2 |
Nagabhushan B. L. |
FLIGHT MECHANICS AND CONTROL CHARACTERISTICS OF A MODERN V/STOL AIRSHIP |
ICAS-98-2.11.1 |
Nagayasu M. |
FLIGHT TESTING OF ALFLEX GUIDANCE, NAVIGATION AND CONTROL SYSTEM |
ICAS-98-1.1.3 |
Naida M. A. |
AERODYNAMIC CHARACTERISTICS OF AXISYMMETRIC AND THREE-DIMENSIONAL BODIES AT TRANSONIC SPEEDS |
ICAS-98-2.4.5 |
Nakayasu H. |
FLIGHT TESTING OF ALFLEX GUIDANCE, NAVIGATION AND CONTROL SYSTEM |
ICAS-98-1.1.3 |
Nakazono Y. |
THE EFFECTS OF CAVITY RESONANCE ON THE MIXING OF RECTANGULAR JETS |
ICAS-98-P11 |
Nangia R. K. |
VECTORING JETS INFLUENCE ON UNDER-WING STORES RELEASE TRAJECTORIES WITH AND WITHOUT SIDE-SLIP EFFECTS, THEORY AND EXPERIMENT |
ICAS-98-3.5.3 |
Nasuti F. |
EVALUATION OF VARIABLE STRUCTURE METHODS FOR AUTOPILOT DESIGN OF AGILE MISSILES |
ICAS-98-1.6.4 |
Neiland V. Y. |
ANALYTICAL AND EXPERIMENTAL INVESTIGATIONS OF AN IMPROVED AERODYNAMIC ORBITER CONFIGURATION |
ICAS-98-R.1.2 |
Nesterenko G.I. |
ENSURING STRUCTURAL DAMAGE TOLERANCE OF ADVANCED AND AGING AIRCRAFT |
ICAS-98-5.7.4 |
Newill D. B. |
COMMON CORE DEVELOPMENT APPROACH FOR ALLISON T406 / AE FAMILY OF TURBOSHAFT, TURBOPROP, AND TURBOFAN ENGINES |
ICAS-98-5.6.3 |
Nicholls P. K. |
THE SENSITIVITY OF SCT DESIGNS TO AIRFIELD NOISE REQUIREMENTS: AN INVESTIGATION USING MULTIVARIATE OPTIMISATION |
ICAS-98-1.2.1 |
Nicolosi F. |
AERODYNAMIC DESIGN OF HIGH-PERFORMANCE SAILPLANE WING-FUSELAGE COMBINATIONS |
ICAS-98-2.9.2 |
Nicolosi F. |
NUMERICAL, WIND-TUNNEL AND FLIGHT TESTS FOR P92J AND P96 LIGHT AIRCRAFT |
ICAS-98-3.11.2 |
Nitsche W. |
CAPABILITIES OF SURFACE MEASUREMENT TECHNIQUES AND THEIR IMPACT ON MODERN WING-DESIGN AND ASSESSMENT |
ICAS-98-3.3.4 |
Nixon D. |
A METHOD FOR THE RAPID PREDICTION OF UNSTEADY LOADS OVER WINGS AT TRANSONIC SPEEDS |
ICAS-98-4.6.1 |
Nordstrom J. |
ACCURACY OF UNSTEADY TRANSONIC FLOW COMPUTATIONS |
ICAS-98-2.4.2 |
Norgia L. |
A NEW NUMERICAL TOOL FOR THE EVALUATION OF NOISE IMPACT GENERATED BY HELICOPTERS |
ICAS-98-5.11.2 |
Nsi Mba |
3D BOUNDARY-LAYER ON ROTATING WINGS: EXPERIMENTS AND CALCULATIONS |
ICAS-98-3.1.1 |
Obermeier E. |
EUROFIGHTER TECHNOLOGY FOR THE 21ST CENTURY |
ICAS-98-0.4 (General Lecture III) |
O'Byrne S. |
PLIF IMAGING OF THE SEPARATED REGION BEHIND A CONE IN A HYPERSONIC FLOW |
ICAS-98-3.10.4 |
Oelkers W. |
THE ENVIRONMENTAL CHALLENGE AS CHANCE FOR THE NEXT CENTURY AIRCRAFT DESIGN |
ICAS-98-4.10.3 |
Oesch S. |
SWISS F / A-18 FATIGUE TRACKING SYSTEM |
ICAS-98-5.1.2 |
Ok H. |
USE OF CFD FOR DESIGN VALIDATION OF A TRANSONIC CIVIL TRANSPORT |
ICAS-98-2.3.3 |
Oliva A. P. |
HELICOPTER REDUNDANT STATION KEEPING FLIGHT CONTROL LAW |
ICAS-98-R.1.10 |
Ollerhead J. B. |
ESTIMATION OF CIVIL AIRCRAFT PERFORMANCE AND OPERATING PRACTICES FROM RADAR DATA |
ICAS-98-5.11.1 |
Olson Jacques C. L. |
BOND DURABILITY PERFORMANCE -THE AUSTRALIAN SILANE SURFACE TREATMENT |
ICAS-98-5.3.1 |
Onischik I. I. |
EXPERIMENTAL INVESTIGATION OF WORKING PROCESS OF THE FRONT DEVICES WITH OPPOSITE FLOW TWISTING, WHICH ARE USED IN THE COMBUSTION CHAMBERS WITH REFINED ECOLOGICAL PERFORMANCES |
ICAS-98-5.8.3 |
Onorato M. |
DPIV ANALYSIS OF WALL TURBULENT SHEAR FLOWS |
ICAS-98-3.1.2 |
Onorato M. |
SKIN FRICTION MEASUREMENTS DOWNSTREAM OF A BACK-FACING STEP |
ICAS-98-3.10.3 |
Orloff K. L. |
AN IMPROVED TECHNIQUE FOR FLIGHT PATH AND GROUNDSPEED ANALYSIS USING RECORDED RADAR DALA |
ICAS-98-6.5.3 |
Ottens H. H. |
FULL-SCALE FUSELAGE PANEL TESTS |
ICAS-98-5.1.1 |
Ozerciyes V. |
FREE FLEXURAL VIBRATIONS OF COMPOSITE PLATES OR PANELS STIFFENED BY A CENTRAL OR NON-CENTRAL PLATE STRIP - SOME COMPARISONS |
ICAS-98-R.4.11 |
Paglione P. |
A PASSIVE AERODYNAMIC STABILIZATION SYSTEM OF SATELLITES FOR LOW EARTH ORBIT: AN ANALYTICAL APPROACH |
ICAS-98-1.3.4 |
Paglione P. |
FUZZY STABILITY AUGMENTATION SYSTEM FOR AIRCRAFT HANDLING QUALITIES |
ICAS-98-1.10.4 |
Palffy S. |
OBLIQUE GROOVES AVOIDING LAMINAR FLOW SEPARATION ON BODIES IN POSITIVE PRESSURE GRADIENTS |
ICAS-98-3.4.4 |
Palma P. C. |
PLIF IMAGING OF THE SEPARATED REGION BEHIND A CONE IN A HYPERSONIC FLOW |
ICAS-98-3.10.4 |
Palmieri D. |
NUMERICAL SIMULATION OF FLUID-STRUCTURE INTERACTION IN AIRCRAFT FUEL TANKS SUBJECTED TO HYDRODYNAMIC RAM PENETRATION |
ICAS-98-4.3.1 |
Pang F. Z. |
A NEW MODEL FOR CREEP OF STITCHED AND UNSTITCHED WOVEN COMPOSITES |
ICAS-98-P12 |
Papadopoulos C. |
AIRCRAFT LANDING-A TOTAL SYSTEM APPROACH |
ICAS-98-1.11.2 |
Paraschivoiu I. |
STABILITY ANALYSIS BY THE OS AND PSE APPROACHES: COMPARISONS WITH EXPERIMENTS |
ICAS-98-2.8.1 |
Parr T. P. |
ACTIVE COMBUSTION CONTROL FOR PROPULSION SYSTEMS |
ICAS-98-5.8.2 |
Patek Z. |
AERODYNAMIC CHARACTERISTICS OF UNCONVENTIONAL AIRCRAFT CONFIGURATIONS |
ICAS-98-3.8.3 |
Patil M. J. |
AEROELASTIC TAILORING OF COMPOSITE BOX BEAMS |
ICAS-98-7.7.5 |
Patil M. J. |
NONLINEAR AEROELASTICITY AND FLIGHT DYNAMICS OF AIRCRAFT IN SUBSONIC FLOW |
ICAS-98-7.7.4 |
Peace A. J. |
SIMULATING THREE DIMENSIONAL AERONAUTICAL FLOWS ON MIXED BLOCK-STRUCTURED/SEMI STRUCTURED / UNSTRUCTURED MESHES |
ICAS-98-2.7.1 (Invited paper) |
Pearce P. J. |
BOND DURABILITY PERFORMANCE -THE AUSTRALIAN SILANE SURFACE TREATMENT |
ICAS-98-5.3.1 |
Pelegrin M. |
TOWARDS AUTOMATED AIRCRAFT'S TAXIING PHASES |
ICAS-98-6.5.2 |
Pendaries C. |
FROM THE HALE GNOPTER TO THE ORNITHOPTER- OR HOW TO TAKE ADVANTAGE OF AIRCRAFT FLEXIBILITY |
ICAS-98-7.2.1 |
Pereira J. C. F. |
LARGE-EDDY SIMULATION OF A TRAILING VORTEX SYSTEM BEHIND A CIVIL AIRCRAFT MODEL |
ICAS-98-2.10.2 |
Periaux J. |
MULTI-OBJECTIVE STRATEGIES FOR COMPLEX OPTIMIZATION PROBLEMS IN AERODYNAMICS USING GENETIC ALGORITHMS |
ICAS-98-2.9.1 |
Perkins S. C. |
PREDICTION OF HIGH-? AERODYNAMIC CHARACTERISTICS OF MANEUVERING AIRCRAFT |
ICAS-98-1.7.5 |
Peshkin D. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Petiau C. |
FROM STRUCTURAL OPTIMIZATION TO MULTIDISCIPLINARY AND MULTILEVEL OPTIMIZATION |
ICAS-98-4.7.1 |
Peto J. W. |
VECTORING JETS INFLUENCE ON UNDER-WING STORES RELEASE TRAJECTORIES WITH AND WITHOUT SIDE-SLIP EFFECTS, THEORY AND EXPERIMENT |
ICAS-98-3.5.3 |
Petretti A. |
NONLINEAR PILOT IN THE LOOP PERFORMANCE USING A MODIFIED CROSSOVER MODEL |
ICAS-98-6.3.2 |
Phillips N. T. J. |
A TIME-MARCHING, TYPE-DEPENDENT, FINITE DIFFERENCE ALGORITHM FOR THE MODIFIED TRANSONIC SMALL DISTURBANCE EQUATION |
ICAS-98-2.6.4 |
Pineiro L. Ferm M. |
APPLICATION OF GROUND COLLISION AVOIDANCE SYSTEM NUISANCE CRITERIA |
ICAS-98-1.8.3 |
Pokoradi l. |
AIRCRAFT OPERATIONAL MANAGEMENT BASED ON STATE-ESTIMATION |
ICAS-98-6.6.3 |
Polidoro R. |
ENGINE SUB-IDLE MODEL |
ICAS-98-5.6.2 |
Post W. |
HUMAN FACTORS MODELS AND CLASSIFICATION SCHEMES FOR IMPROVING OCCURENT DATA REPORTING SYSTEMS |
ICAS-98-1.9.4 |
Prabhakaran V. |
PROBABILISTIC APPROACH FOR DESIGN OF A COMPOSITE RPV WING |
ICAS-98-R.4.7 |
Prabhakaran Y. |
PROBABILISTIC APPROACH FOR DESIGN OF A COMPOSITE RPVWING. |
ICAS-98-5.9.4 |
Prananta B. B. |
COMPUTATIONAL UNSTEADY AERODYNAMICS IN AEROELASTIC SIMULATION |
ICAS-98-4.6.3 |
Pruis G. W. |
FROM A MONO-DISCIPLINARY TO A MULTI-DISCIPLINARY APPROACH IN AEROSPACE: AS SEEN FROM AN INFORMATION AND COMMUNICATION TECHNOLOGY PERSPECTIVE |
ICAS-98-6.8.2 |
Qi Y. J. |
GRADATION OF DMMH/FH INDEX, A RESEARCH ON AIRCRAFT MAINTAINABILITY EVALUATION INDEX |
ICAS-98-P13 |
Qiao J. J. |
MACHINERY STRENGTH AND DAMAGE TOLERANCE ANALYSIS ON MAGNALIUM WHEEL |
ICAS-98-P14 |
Quagliotti F. B. |
A STUDY OF SELF INDUCED OSCILLATORY ROLLING MOTION: ANALYTICAL AND EXPERIMENTAL RESULTS |
ICAS-98-1.7.2 |
Quagliotti F. B. |
EFFECT OF MAIN ROTOR CONFIGURATION AND PROPULSION SYSTEM DYNAMICS ON HELICOPTER HANDLING QUALITIES |
ICAS-98-1.4.1 |
Querzoli R. |
SAFETY ASSESSMENT OF AIRCRAFT MOUNTED SYSTEMS |
ICAS-98-6.7.3 |
Raghunathan S. |
A PROPOSITION IN DESIGN EDUCATION WITH A POTENTIAL IN COMMERCIAL VENTURE IN SMALL AIRCRAFT MANUFACTURE |
ICAS-98-6.4.1 |
Rajaiah K. |
PROBABILISTIC APPROACH FOR DESIGN OF A COMPOSITE RPVWING. |
ICAS-98-5.9.4 |
Rasuo B. |
AN EXPERIMENTAL AND THEORETICAL STUDY OF TRANSONIC FLOW ABOUT THE NACA 0012 AIRFOIL |
ICAS-98-R.3.8 |
Rasuo B. |
EFFECT OF LOAD FACTORS ON TURN MANOEUVER OF AGRICULTURAL AIRCRAFT |
ICAS-98-2.11.3 |
Reda D. C. |
QUANTITATIVE AND QUALITATIVE ASPECTS OF THE SHEAR-SENSITIVE LIQUID CRYSTAL COATING METHOD |
ICAS-98-3.3.2 |
Rees P. H. |
AERODYNAMIC DESIGN OPTIMISATION APPLIED TO CIVIL TRANSPORTS WITH UNDERWING MOUNTED ENGINES |
ICAS-98-2.3.1 |
Ren H. |
THE METHOD FOR COMPUTING THE FAILURE PROBABILITY OF AIRCRAFT STRUCTURES |
ICAS-98-R.5.7 |
Renzoni P. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Rhodes D. P. |
DEVELOPMENT OF AN INTEGRATED CONCEPTUAL AIRCRAFT DESIGN AND AIRCRAFT NOISE MODEL FOR CIVIL TRANSPORT AIRCRAFT |
ICAS-98-6.4.3 |
Rhodes D.P. |
ESTIMATION OF CIVIL AIRCRAFT PERFORMANCE AND OPERATING PRACTICES FROM RADAR DATA |
ICAS-98-5.11.1 |
Riabov V. V. |
AEROTHERMODYNAMIC CHARACTERISTICS OF TWO-DIMENSIONAL BLUFF BODIES IN HYPERSONIC VISCOUS FLOWS |
ICAS-98-R.2.1 |
Ricci F. |
NUMERICAL, WIND-TUNNEL AND FLIGHT TESTS FOR P92J AND P96 LIGHT AIRCRAFT |
ICAS-98-3.11.2 |
Ricci S. |
STRUCTURAL DAMAGE DETECTION USING BEST ACHIEVABLE "MODAL" EIGENVECTORS |
ICAS-98-4.3.2 |
Rider A. N. |
BOND DURABILITY PERFORMANCE -THE AUSTRALIAN SILANE SURFACE TREATMENT |
ICAS-98-5.3.1 |
Righi M. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Rinoie K. |
BEHAVIOURS OF SEPARATED AND REATTACHING FLOW FORMED OVER BACKWARD FACING STEP |
ICAS-98-3.10.2 |
Rinoie K. |
EXPERIMENTS ON DELTA WINGS WITH ROUNDED LEADING-EDGE VORTEX FLAPS |
ICAS-98-3.6.1 |
Ripamonti S. |
HIRF /EMC TEST TECHNOLOGIES AND METHODOLOGIES |
ICAS-98-1.11.3 |
Risdaya Fadil M. |
N-2S0 PROTOTYPE 1 FLIGHT FLUTTER TESTING DEVELOPMENT |
ICAS-98-4.5.3 |
Risitc S. |
ANALYSIS OF THE ACCURACY OF THE THIRD COMPONENT OF FLOW VELOCITY MEASUˇ REMENTS FOR 3-COMPONENT, 3-COLOR LASER DOPPLER ANEMOMETER |
ICAS-98-P15 |
Robinson G. |
VECTORING JETS INFLUENCE ON UNDER-WING STORES RELEASE TRAJECTORIES WITH AND WITHOUT SIDE-SLIP EFFECTS, THEORY AND EXPERIMENT |
ICAS-98-3.5.3 |
Rodzewicz M. |
SOME INVESTIGATIONS ON WOOD-COMPOSITE STRUCTURES FOR VERY LIGHT AIRCRAFT (VLA) |
ICAS-98-4.4.4 |
Roeder J. |
THE ECOLIFTER : A NEW CONCEPT FOR A DEDICATED ADVANCED CARGO TRANSPORT |
ICAS-98-4.10.1 |
Rohacs J. |
A SENSITIVITY ANALYSIS OF CHAOS AT HIGH ANGLE OF ATTACK |
ICAS-98-1.7.3 |
Rohacs J. |
UNCONVENTIONAL FLIGHT ANALYSIS |
ICAS-98-1.4.3 |
Rollin C. |
ENGINE INTEGRATION ON FUTURE TRANSPORT AIRCRAFT - THE EUROPEAN RESEARCH PROGRAMMES DUPRIN/ENIFAIR |
ICAS-98-5.6.1 |
Romeo G. |
EXPERIMENTAL BEHAVIOR OF GRAPHITE / EPOXY PANELS WITH CUT-OUTS UNDER BIAXIAL TENSION, COMPRESSION AND SHEAR LOADS |
ICAS-98-4.4.2 |
Romeo G. |
MANUFACTURING AND TESTING OF GRAPHITE-EPOXY WING BOX AND FUSELAGE STRUCTURES FOR A SOLARPOWERED UAV-HAVE |
ICAS-98-4.4.5 |
Roots M. |
THE ROYAL AIR FORCE CHINOOK HELICOPTER SNOW AND ICING FLIGHT ENVELOPE EXPANSION |
ICAS-98-P16 |
Rose L. F. R. |
ANALYSIS OF THE INTERACTION EFFECT FOR BONDED REPAIRS |
ICAS-98-R.5.3 |
Ross J. A |
VECTORING JETS INFLUENCE ON UNDER-WING STORES RELEASE TRAJECTORIES WITH AND WITHOUT SIDE-SLIP EFFECTS, THEORY AND EXPERIMENT |
ICAS-98-3.5.3 |
Rossow C. |
ENGINE INTEGRATION ON FUTURE TRANSPORT AIRCRAFT - THE EUROPEAN RESEARCH PROGRAMMES DUPRIN/ENIFAIR |
ICAS-98-5.6.1 |
Rossow C. C. |
MEGAFLOW -A NUMERICAL FLOW SIMULATION SYSTEM |
ICAS-98-2.7.4 |
Rouwhorst W. F. J. A. |
EVALUATION OF WINDSHEAR HAZARD DISPLAYS AND GO-AROUND PROCEDURES USING PILOTED SIMULATIONS AT NLR |
ICAS-98-6.7.2 |
Ruigrok R. C. J. |
COCKPIT SYSTEMS REQUIREMENTS IN A FUTURE ATM ENVIRONMENT |
ICAS-98-6.2.2 |
Ruotolo R. |
ON-LINE HEALTH MONITORING OF AERONAUTICAL STRUCTURES USING A VIBRATION BASED METHOD |
ICAS-98-R.5.1 |
Ruotolo R. |
OPTIMAL PLACEMENT OF PIEZOELECTRIC SENSORS AND ACTUATORS USING COMBINATORIAL OPTIMISATION |
ICAS-98-4.11.2 |
Russel T. |
PERFORMANCE FLIGHT TESTING OF AN F-111 C AIRCRAFT |
ICAS-98-1.1.1 |
Rutovskiy V. B. |
EXPERIMENTAL INVESTIGATION OF WORKING PROCESS OF THE FRONT DEVICES WITH OPPOSITE FLOW TWISTING, WHICH ARE USED IN THE COMBUSTION CHAMBERS WITH REFINED ECOLOGICAL PERFORMANCES |
ICAS-98-5.8.3 |
Ryzhova T. B. |
ULTRASONIC ASSESSMENT OF THE RADIAL CLEARANCE OF RIVETED JOINTS IN AIRCRAFT STRUCTURES |
ICAS-98-R.4.2 |
Sachs G. |
OPTIMAL THREE-DIMENSIONAL RANGE CRUISE OF A DUAL-FUEL HYPERSONIC VEHICLE |
ICAS-98-1.3.1 |
Saito Y. |
BEHAVIOURS OF SEPARATED AND REATTACHING FLOW FORMED OVER BACKWARD FACING STEP |
ICAS-98-3.10.2 |
Saitoh K. |
NONLINEAR CHARACTERISTICS OF TRANSONIC FLUTTER OF A HIGH ASPECT RATIO WING |
ICAS-98-4.1.2 |
Sakya A. E. |
COMMEMORATING TEN YEARS OPERATION OF THE INDONESIAN LOW SPEED TUNNEL (ILST) |
ICAS-98-3.11.3 |
Salbut L. |
SOME INVESTIGATIONS ON WOOD-COMPOSITE STRUCTURES FOR VERY LIGHT AIRCRAFT (VLA) |
ICAS-98-4.4.4 |
Sanderson S. |
ANALYSIS OF THE INTERACTION EFFECT FOR BONDED REPAIRS |
ICAS-98-R.5.3 |
Sanderson S. |
DEVELOPMENT OF AN ANALYTICAL EXPRESSION AND A FINITE ELEMENT PROCEDURE TO DETERMINE THE RESIDUAL STRESSES IN BONDED REPAIRS |
ICAS-98-4.8.3 |
Santini P. |
NUMERICAL SIMULATION OF FLUID-STRUCTURE INTERACTION IN AIRCRAFT FUEL TANKS SUBJECTED TO HYDRODYNAMIC RAM PENETRATION |
ICAS-98-4.3.1 |
Sanz A. |
THE EVOLUTION UNDER STRESS OF THE SUPERALLOY / PROTECTIVE COATING INTERFACE |
ICAS-98-4.2.2 |
Saravanan P. M. |
PROBABILISTIC APPROACH FOR DESIGN OF A COMPOSITE RPV WING |
ICAS-98-R.4.7 |
Saravanan P. M. |
PROBABILISTIC APPROACH FOR DESIGN OF A COMPOSITE RPVWING. |
ICAS-98-5.9.4 |
Sarma G. R. |
IN-FLIGHT SHOCK DETECTION USING HOT FILM SENSORS AND CONSTANT VOLTAGE ANEMOMETER SYSTEM |
ICAS-98-3.3.3 |
Sarychev V. A. |
A PASSIVE AERODYNAMIC STABILIZATION SYSTEM OF SATELLITES FOR LOW EARTH ORBIT: AN ANALYTICAL APPROACH |
ICAS-98-1.3.4 |
Sayce A. |
THE RISKS OF OVERRUNS |
ICAS-98-1.11.1 |
Sbuttoni A. |
ENGINE SUB-IDLE MODEL |
ICAS-98-5.6.2 |
Schadow K. C. |
ACTIVE COMBUSTION CONTROL FOR PROPULSION SYSTEMS |
ICAS-98-5.8.2 |
Schmitt D. |
THE ECOLIFTER : A NEW CONCEPT FOR A DEDICATED ADVANCED CARGO TRANSPORT |
ICAS-98-4.10.1 |
Schneegans A. |
FLYING OBJECTS - AN OBJECT-ORIENTED TOOLBOX FOR MULTIDISCIPLINARY DESIGN AND EVALUATION OF AIRCRAFT |
ICAS-98-6.4.4 |
Schnellbeck A |
INTEGRATED FLIGHT AND PAYLOAD CONTROL FOR DIRECTIONAL PAYLOADS ON UAVS |
ICAS-98-3.7.2 |
Schoell E. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Schumacher J. |
THE ENVIRONMENTAL CHALLENGE AS CHANCE FOR THE NEXT CENTURY AIRCRAFT DESIGN |
ICAS-98-4.10.3 |
Schutte P. C. |
FUTURE FLIGHT DECKS |
ICAS-98-1.9.3 |
Scott M. L. |
INVESTIGATION OF SHAPE OPTIMISATION TECHNIQUES FOR THE DESIGN OF PLATES WITH CUT-OUTS |
ICAS-98-4.7.5 |
Scott M. L. |
THE EFFECT OF DAMAGE ON THE PERFORMANCE OF POSTBUCKLING FIBRE COMPOSITE SHEAR PANELS |
ICAS-98-5.9.2 |
Searl A. |
INVESTIGATION OF SHAPE OPTIMISATION TECHNIQUES FOR THE DESIGN OF PLATES WITH CUT-OUTS |
ICAS-98-4.7.5 |
Searl A. |
THROUGH-THICKNESS STRESSES IN AIRCRAFT BONDED JOINTS |
ICAS-98-4.3.4 |
Sedin Y. C. -J. |
COMPUTATION OF WIND TUNNEL FLOWS IN TRANSONIC SLOTTED-WALL TEST SECTIONS |
ICAS-98-3.11.1 |
Seebass R. |
MANUAL AERODYNAMIC OPTIMIZATION OF OBLIQUE FLYING WING |
ICAS-98-2.1.3 |
Sefrioui M. |
MULTI-OBJECTIVE STRATEGIES FOR COMPLEX OPTIMIZATION PROBLEMS IN AERODYNAMICS USING GENETIC ALGORITHMS |
ICAS-98-2.9.1 |
Sekar W. K. |
A NUMERICAL STUDY OF LIFTING SURFACE AEROELASTIC INSTABILITY USING TRANSONIC UNSTEADY AERODYNAMIC CODE -NTRANS |
ICAS-98-4.6.2 |
Self A. W. |
AIRCRAFT LANDING-A TOTAL SYSTEM APPROACH |
ICAS-98-1.11.2 |
Shankar K. |
LOAD TRANSFER MECHANISM IN BOLTED DOUBLE LAP JOINTS |
ICAS-98-5.3.3 |
Shapovalov G. K. |
EXPERIMENTAL INVESTIGATION ON THE APPLICATION OF HYBRID LAMINAR FLOW CONTROL TO LARGE-SCALE SWEPT WING MODELS AT SUBSONIC SPEEDS |
ICAS-98-3.4.2 |
Sharp P. K. |
THE INFLUENCE OF CORROSION ON AIRCRAFT STRUCTURAL INTEGRITY |
ICAS-98-5.2.1 |
Shaw J. A. |
SIMULATING THREE DIMENSIONAL AERONAUTICAL FLOWS ON MIXED BLOCK-STRUCTURED/SEMI STRUCTURED / UNSTRUCTURED MESHES |
ICAS-98-2.7.1 (Invited paper) |
Shen G. |
A NEW, AVAILABLE HIGH-PRECISION CCD ANGLE-MEASURING SENSOR IN AERONAUTICS AND ASTRONAUTICS |
ICAS-98-R.5.11 |
Sherwood T. |
PREDICTION OF ANTISYMMETRIC BUFFET LOADS ON HORIZONTAL STABILIZERS IN MASSIVELY SEPARATED FLOWS |
ICAS-98-4.1.1 |
Shirai Y. |
BEHAVIOURS OF SEPARATED AND REATTACHING FLOW FORMED OVER BACKWARD FACING STEP |
ICAS-98-3.10.2 |
Shires A. |
TRAILING-EDGE FLOWS ON HIGHLY-SWEPT WINGS |
ICAS-98-3.8.1 |
Siguerdidjane H. B. |
TOWARDS AUTOMATED AIRCRAFT'S TAXIING PHASES |
ICAS-98-6.5.2 |
Sijp J. C. |
INVESTIGATION INTO THE FORMATION OF WAVES ON THIN LAYERS OF DE-/ ANTI-ICING FLUIDS ON WINGS |
ICAS-98-7.1.1 |
Sjoberg J. |
VORTICITY MEASUREMENTS IN THE NEAR-FIELD OF A WING TIP VORTEX |
ICAS-98-3.2.2 |
Skibniewski F. |
APPLICATION OF A FLIGHT SIMULATOR FOR SELECTION OF PILOT-CANDIDATES |
ICAS-98-6.3.3 |
Skoog M. |
APPLICATION OF GROUND COLLISION AVOIDANCE SYSTEM NUISANCE CRITERIA |
ICAS-98-1.8.3 |
Smalko Z. |
APPLICATION OF EXPERT METHODS TO RISK ASSESSMENT OF AIR TRANSPORT SYSTEMS |
ICAS-98-R.1.9.2 |
Smith P. |
THE EFFECT OF MATRIX MOISTURE CONTENT ON THE REPAIR OF CARBON FIBRE REINFORCED EPOXY |
ICAS-98-4.4.3 |
Smrcek L. |
AERODYNAMIC CHARACTERISTICS OF UNCONVENTIONAL AIRCRAFT CONFIGURATIONS |
ICAS-98-3.8.3 |
Smrcek L. |
WIND TUNNEL LNVESTIGATIONS ON RPV WING GLOVE CONFIGURATION |
ICAS-98-3.7.4 |
Snowden A. |
PERFORMANCE FLIGHT TESTING OF AN F-111 C AIRCRAFT |
ICAS-98-1.1.1 |
Sobieczky H. |
MANUAL AERODYNAMIC OPTIMIZATION OF OBLIQUE FLYING WING |
ICAS-98-2.1.3 |
Sodzi P. |
THE DYNAMIC MODES AND NATURAL FREQUENCIES OF OVERHEAD STOWAGES IN TRANSPORT AIRCRAFT |
ICAS-98-4.1.4 |
Soijer M. W. |
COMPREHENSIVE TIME ANALYSIS IN AEROELASTIC SIMULATIONS |
ICAS-98-4.3.3 |
Song B. F. |
THE METHOD FOR COMPUTING THE FAILURE PROBABILITY OF AIRCRAFT STRUCTURES |
ICAS-98-R.5.7 |
Sousa J. M. M. |
LARGE-EDDY SIMULATION OF A TRAILING VORTEX SYSTEM BEHIND A CIVIL AIRCRAFT MODEL |
ICAS-98-2.10.2 |
Spazzini P. G. |
SKIN FRICTION MEASUREMENTS DOWNSTREAM OF A BACK-FACING STEP |
ICAS-98-3.10.3 |
Srinivasan S. |
FAILURE CRITERIA FOR THE THICK GRP COMPOSITE STRUCTURES CONTAINING DELAMINATIONS AND POROSITY |
ICAS-98-P17 |
Starkey R. P. |
A SIMPLE ANALYTICAL MODEL FOR PARAMETRIC STUDIES OF HYPERSONIC WAVERIDERS |
ICAS-98-7.3.1 |
Stengele I. |
DEVELOPMENT, QUALIFICATION AND FLIGHT TESTING OF A WINGGRID ON A JET-POWERED TESTBED |
ICAS-98-1.1.4 |
Sterling G. |
ANALYSIS AND DESIGN 01 SYNTNETIC ENVIRONMENTS FOR MULTIPLE SENSOR SYSTEMS |
ICAS-98-P18 |
Sterling S. G. |
A DESIGN AND TEST PROGRAMME INVOLVING WELDED SHEET-STRINGER COMPRESSION PANELS |
ICAS-98-7.7.3 |
Sterling S. G. |
A FINITE ELEMENT STUDY OF THE POST-BUCKLING BEHAVIOUR OF A FLAT STIFFENED PANEL |
ICAS-98-7.7.2 |
Stocker D. P. |
CHARACTERISTICS OF MOMENTUM-DOMINATED HYDROCARBON TURBULENT DIFFUSION FLAMES |
ICAS-98-5.8.1 |
Stocks G. J. |
PREDICTION OF FATIGUE CRACK GROWTH FROM BOLT HOLES IN A TITANIUM DISC |
ICAS-98-5.2.3 |
Strauss D. |
AXISYMETRIC SIMULATIONS OF TURBULENT COMPRESSIBLE FLOWS OVER AEROSPACE VEHICLES |
ICAS-98-2.8.3 |
Strohmeyer D. |
EXPERIMENTAL AND NUMERICAL INVESTIGATIONS ON WAVERIDERS IN DIFFERENT FLIGHT REGIMES |
ICAS-98-2.1.4 |
Sullivan P. |
LUMINESCENT PAINT TECHNOLOGY FOR TEMPERATURE AND PRESSURE MEASUREMENTS IN A CRYOGENIC WIND TUNNEL |
ICAS-98-3.3.1 |
Sunada Y. |
BEHAVIOURS OF SEPARATED AND REATTACHING FLOW FORMED OVER BACKWARD FACING STEP |
ICAS-98-3.10.2 |
Sung B. |
USE OF CFD FOR DESIGN VALIDATION OF A TRANSONIC CIVIL TRANSPORT |
ICAS-98-2.3.3 |
Surace C. |
ON-LINE HEALTH MONITORING OF AERONAUTICAL STRUCTURES USING A VIBRATION BASED METHOD |
ICAS-98-R.5.1 |
Surace G. |
HUMAN FACTORS MODELS AND CLASSIFICATION SCHEMES FOR IMPROVING OCCURENT DATA REPORTING SYSTEMS |
ICAS-98-1.9.4 |
Surace G. |
OPTIMAL PLACEMENT OF PIEZOELECTRIC SENSORS AND ACTUATORS USING COMBINATORIAL OPTIMISATION |
ICAS-98-4.11.2 |
Suttan J. |
CAPABILITIES OF SURFACE MEASUREMENT TECHNIQUES AND THEIR IMPACT ON MODERN WING-DESIGN AND ASSESSMENT |
ICAS-98-3.3.4 |
Swan G. |
BOND DURABILITY PERFORMANCE -THE AUSTRALIAN SILANE SURFACE TREATMENT |
ICAS-98-5.3.1 |
Swan G. |
THE EFFECT OF MATRIX MOISTURE CONTENT ON THE REPAIR OF CARBON FIBRE REINFORCED EPOXY |
ICAS-98-4.4.3 |
Swihart D. E. |
RESULTS OF A JOINT US/SWEDISH AUTO GROUND COLLISION AVOIDANCE SYSTEM PROGRAM |
ICAS-98-1.8.2 |
Szabolcsi R. |
AIRCRAFT OPERATIONAL MANAGEMENT BASED ON STATE-ESTIMATION |
ICAS-98-6.6.3 |
Sznajder J. |
ANALYSIS OF TRANSIENT DYNAMIC BEHAVIOUR OF A FIRE FIGHTING AIRCRAFT AFTER THE WATER BOMB DROPPING |
ICAS-98-1.4.4 |
Szodruch J. |
THE ENVIRONMENTAL CHALLENGE AS CHANCE FOR THE NEXT CENTURY AIRCRAFT DESIGN |
ICAS-98-4.10.3 |
Taghavi R. R. |
SUPERSONIC UNDEREXPANDED RECTANGULAR JET OSCILLATIONS: A COMPUTATIONAL STUDY |
ICAS-98-2.10.5 |
Tahiri V. |
NUMERICAL MODELLING FOR PREDICTING DAMAGE TOLERANCE OF COMPOSITE STRUCTURE |
ICAS-98-5.9.3 |
Talamelli A. |
VORTICITY MEASUREMENTS IN THE NEAR-FIELD OF A WING TIP VORTEX |
ICAS-98-3.2.2 |
Talbot-Stern J. L. |
DIRECT SIMULATION (MONTE CARLO) OF DELTA WINGS IN THREE-DIMENSIONAL, NEAR-CONTINUUM, SUBSONIC FLOWS |
ICAS-98-R.2.2 |
Tanaka T. |
MISSILE GUIDANCE LAW BY NEURAL NETWORK AND GENETIC ALGORITHM |
ICAS-98-P19 |
Tao B. -Q. |
RESEARCH OF ACTIVE VIBRATION CONTROL TECHNOLOGIES FOR A COMPOSITE SHELL |
ICAS-98-4.11.1 |
Tarnopolsky A. Z. |
MIXING DUE TO A SUPERSONIC MAIN STREAM AND CO-FLOWING SUPERSONIC PARALLEL JET |
ICAS-98-3.5.2 |
Tchernycheva O. V. |
NON-REFLECTING BOUNDARY CONDITIONS FOR NON-LINEAR EULER CALCULATIONS USING AN IMPLICIT APPROACH |
ICAS-98-7.4.4 |
Tenney D. R. |
AIRFRAME SYSTEMS TECHNOLOGIES FOR THE 21ST CENTURY |
ICAS-98-0.2 (General Lecture I) |
Terborg G. |
FINITE ELEMENT MODELING AND EXPERIMENTAL STUDY OF A GAS TURBINE ENGINE BLADE UNDER BIAXIAL LOADING |
ICAS-98-5.1.4 |
Thepot R. |
ONERA ACTIVITIES ON SUPERSONIC TRANSPORT AIRCRAFT AERODYNAMICS |
ICAS-98-2.1.2 |
Thibert J. J. |
ONERA ACTIVITIES ON SUPERSONIC TRANSPORT AIRCRAFT AERODYNAMICS |
ICAS-98-2.1.2 |
Thiele F. |
MEGAFLOW -A NUMERICAL FLOW SIMULATION SYSTEM |
ICAS-98-2.7.4 |
Thomson D. G. |
ESTIMATION OF PILOT MODEL PARAMETERS FOR HELICOPTER HANDLING QUALITIES STUDIES |
ICAS-98-R.6.3 |
Thomson R. S. |
INVESTIGATION OF SHAPE OPTIMISATION TECHNIQUES FOR THE DESIGN OF PLATES WITH CUT-OUTS |
ICAS-98-4.7.5 |
Thomson R. S. |
THE EFFECT OF DAMAGE ON THE PERFORMANCE OF POSTBUCKLING FIBRE COMPOSITE SHEAR PANELS |
ICAS-98-5.9.2 |
Tohboh K. |
A SIDE FORCE CONTROLLER USING VARIABLE PLUG NOZZLES |
ICAS-98-P20 |
Tong X. |
NUMERICAL SIMULATION OF THE TEMPERATURE FIELD DURING FATIGUE PROCESS |
ICAS-98-7.7.1 |
Tran-Cong T. |
DEVELOPMENT OF AN ANALYTICAL EXPRESSION AND A FINITE ELEMENT PROCEDURE TO DETERMINE THE RESIDUAL STRESSES IN BONDED REPAIRS |
ICAS-98-4.8.3 |
Tropis A. |
NUMERICAL MODELLING FOR PREDICTING DAMAGE TOLERANCE OF COMPOSITE STRUCTURE |
ICAS-98-5.9.3 |
Trotta L. |
SAFETY ASSESSMENT OF AIRCRAFT MOUNTED SYSTEMS |
ICAS-98-6.7.3 |
Tsao D. |
EFFECTS OF STRETCHING-BENDING COUPLINGS ON THE BUCKLING AND THERMAL BUCKLING BEHAVIOR OF UNSYMMETRIC LAMINATES |
ICAS-98-4.8.2 |
Tuncer I. H. |
AN INVERSE DESIGN PROCEDURE FOR AIRFOILS USING ARTIFICIAL NEURAL NETWORKS |
ICAS-98-2.2.1 |
Tung X. Y. |
THE DESIGN OF USER-ORIENTED FATIGUE DATABASE BASED ON CLIENT/SERVER MODEL |
ICAS-98-7.5.3 |
Turner R. |
RESULTS OF A JOINT US/SWEDISH AUTO GROUND COLLISION AVOIDANCE SYSTEM PROGRAM |
ICAS-98-1.8.2 |
Tysell L. |
A MULTIGRID ALGORITHM FOR INVISCID FLOW COMPUTATIONS ON UNSTRUCTURED GRIDS |
ICAS-98-2.7.3 |
Urbanski M. |
DETERMINATION OF FLIGHT-SAFETY RATES AND EXAMINATION OF THEIR VARIATIONS WITH TIME IN CORRELATION TO RELIABILITY RATES |
ICAS-98-6.7.4 |
Valentinis F. |
A TOOLSET FOR THE DESIGN OF AUTONOMOUS UAV SYSTEMS |
ICAS-98-3.7.3 |
van Beek B. |
DYNAMIC SEAT AND HEAD INJURY CRITERIA: ON AIRCRAFT MANUFACTURERS EXPERIENCE AND A VIEW ON THE FUTURE |
ICAS-98-P21 |
van Beek J. A. B. |
DYNAMIC SEAT TESTING AND HEAD INJURY CRITERIA-AN AIRCRAFT MANUFACTURER'S EXPERIENCE AND A VIEW ON THE FUTURE |
ICAS-98-R.4.5 |
van Bronswijk N. |
A COMPARISON OF THREE TECHNIQUES FOR THE PREDICTION OF ISOLATED PROPELLER PERFORMANCE |
ICAS-98-5.10.1 |
van der Veen E. M. |
CIVIL APPLICATIONS OF THRUST VECTORING -AN EXPLORATION |
ICAS-98-7.5.2 |
van Gimst R. F.W. G. |
COCKPIT SYSTEMS REQUIREMENTS IN A FUTURE ATM ENVIRONMENT |
ICAS-98-6.2.2 |
Varga A. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN PART 3: PHYSICAL MODELING OF AIRCRAFT FOR AUTOMATED LFT GENERATION APPLIED TO THE RESEARCH CIVIL AIRCRAFT MODEL |
ICAS-98-1.6.3 |
Varga A. |
ROBUSTNESS ANALYSIS APPLIED TO AUTOPILOT DESIGN. PART I : ?-ANALYSIS OF DESIGN ENTRIES TO A ROBUST FLIGHT CONTROL BENCHMARK |
ICAS-98-1.6.1 |
Vassilopoulos K. |
BOUNDARY LAYER EFFECTS ON THE BASE PRESSURE BEHIND A BLUNT TRAILING EDGE AEROFOIL |
ICAS-98-3.10.5 |
Veldhuis L. L. M. |
A SIMPLE WING OPTIMISATION CODE INCLUDING PROPELLER EFFECTS |
ICAS-98-2.3.4 |
Vellutini M. |
NONLINEAR PILOT IN THE LOOP PERFORMANCE USING A MODIFIED CROSSOVER MODEL |
ICAS-98-6.3.2 |
Vercammen R. W. A |
FULL-SCALE FUSELAGE PANEL TESTS |
ICAS-98-5.1.1 |
Verhoff A. |
EFFICIENCY IMPROVEMENT OF CFD CODES USING ANALYTICAL FAR-FIELD BOUNDARY CONDITIONS |
ICAS-98-2.2.2 |
Vieira R. |
THREE DIMENSIONAL FLOW SIMULATION IN THE TEST SECTION OF A SLOTTED TRANSONIC WIND TUNNEL |
ICAS-98-R.3.11 |
Vigevano L. |
EROS: A EUROPEAN EULER CODE FOR HELICOPTER ROTOR FLOW SIMULATIONS |
ICAS-98-2.6.1 |
Vilenius J. |
CALIBRATION OF AIR COMBAT SIMULATION MODELS BASED ON PERFORMANCE DATA |
ICAS-98-2.11.2 |
Villero G. |
MECHANICAL FAILURES OF FLAP CONTROL SYSTEMS AND RELATED MONITORING TECHNIQUES |
ICAS-98-5.5.2 |
Vogels M. E. S. |
FROM A MONO-DISCIPLINARY TO A MULTI-DISCIPLINARY APPROACH IN AEROSPACE: AS SEEN FROM AN INFORMATION AND COMMUNICATION TECHNOLOGY PERSPECTIVE |
ICAS-98-6.8.2 |
von Tein V. |
STATUS AND TRENDS IN COMMERCIAL TRANSPORT AIRCRAFT |
ICAS-98-0.3 (General Lecture II) |
Vyshinsky V. V. |
AIRCRAFT VORTEX WAKE, FLIGHT SAFETY AND CRISIS OF AIRPORTS |
ICAS-98-6.5.1 |
Wagner S. |
NUMERICAL SHAPE OPTIMIZATION OF NATURAL LAMINAR FLOW BODIES |
ICAS-98-2.9.4 |
Wagner S. |
SIMULATION OF FLUID-STRUCTURE INTERACTION AT THE HELICOPTER ROTOR |
ICAS-98-2.5.1 |
Wagstaff P. G. |
THE INFLUENCE OF CORROSION ON THE FATIGUE AND FRACTURE BEHAVIOUR OF 7050-T76 ALUMINIUM ALLOY SPECIMENS CONTAINING COLD EXPANDED HOLES |
ICAS-98-5.2.2 |
Wahono A. R. |
N2130: A NEW REGIONAL AIRLINER FOR THE 21 ST CENTURY |
ICAS-98-4.10.4 |
Waldman W. |
DYNAMIC LOAD DEVELOPMENT AND RESULTS FOR DYNAMIC EXCITATION OF A FULL-SCALE F/A-18 FATIGUE TEST ARTICLE |
ICAS-98-4.5.1 |
Walker K. |
DEVELOPMENT OF AN ANALYTICAL EXPRESSION AND A FINITE ELEMENT PROCEDURE TO DETERMINE THE RESIDUAL STRESSES IN BONDED REPAIRS |
ICAS-98-4.8.3 |
Walker K. F. |
CRACK GROWTH PREDICTION USING AN ANALYTICAL CRACK CLOSURE MODEL FOR A SEMI-ELLIPTIC SURFACE FLAW LOADED IN COMBINED TENSION AND OUT OF PLANE BENDING |
ICAS-98-5.7.2 |
Wallscheid L. |
ON THE STEADY AND UNSTEADY EFFECTS OF BLADE ROW SPACING IN A COUNTER-ROTATING DUCTED PROPFAN |
ICAS-98-5.4.3 |
Walter S. |
CAST AIRFRAME PRIMARY STRUCTURE |
ICAS-98-R.6.1 |
Wan J. G. |
RESEARCH OF ACTIVE VIBRATION CONTROL TECHNOLOGIES FOR A COMPOSITE SHELL |
ICAS-98-4.11.1 |
Wang C. H. |
NUMERICAL SIMULATION OF FATIGUE CRACK CLOSURE BEHAVIOUR UNDER BIAXIAL LOADING |
ICAS-98-5.7.1 |
Wang C. H. |
PREDICTION OF FATIGUE CRACK GROWTH FROM BOLT HOLES IN A TITANIUM DISC |
ICAS-98-5.2.3 |
Wang D. |
PROPELLER SLIPSTREAM COMPUTATIONAL METHODS |
ICAS-98-2.6.2 |
Wang M. |
THE DESIGN OF USER-ORIENTED FATIGUE DATABASE BASED ON CLIENT/SERVER MODEL |
ICAS-98-7.5.3 |
Wayan Tjatra I. |
A NUMERICAL STUDY OF LIFTING SURFACE AEROELASTIC INSTABILITY USING TRANSONIC UNSTEADY AERODYNAMIC CODE -NTRANS |
ICAS-98-4.6.2 |
Weigelt J. |
TESTING OF AN AUTOMATIC, LOW ALTITUDE, ALL TERRAIN GROUND COLLISION AVOIDANCE SYSTEM |
ICAS-98-1.8.1 |
Welch J. |
TESTING OF AN AUTOMATIC, LOW ALTITUDE, ALL TERRAIN GROUND COLLISION AVOIDANCE SYSTEM |
ICAS-98-1.8.1 |
Wharington J. |
CONTROL OF HIGH ENDURANCE UNMANNED AIR VEHICLE |
ICAS-98-3.7.1 |
Wicks B. J. |
LIFE MANAGEMENT OF AIRCRAFT ENGINE COMPONENTS USING RETIREMENT FOR CAUSE PROCEDURES |
ICAS-98-6.6.1 |
Wilder M. E. |
QUANTITATIVE AND QUALITATIVE ASPECTS OF THE SHEAR-SENSITIVE LIQUID CRYSTAL COATING METHOD |
ICAS-98-3.3.2 |
Williams S. P. |
PNEUMATIC YAW CONTROL AT HIGH ANGLE OF ATTACK FOR LOW OBSERVABILITY COMBAT AIRCRAFT |
ICAS-98-1.10.3 |
Wilmoth R. G. |
MARS ENTRY VEHICLE AERODYNAMIC FLIGHT MEASUREMENTS |
ICAS-98-1.2.3 |
Wilson A. R. |
BOND DURABILITY PERFORMANCE -THE AUSTRALIAN SILANE SURFACE TREATMENT |
ICAS-98-5.3.1 |
Wiriadidjaja S. |
COMMEMORATING TEN YEARS OPERATION OF THE INDONESIAN LOW SPEED TUNNEL (ILST) |
ICAS-98-3.11.3 |
Wong K. C. |
INTEGRATED FLIGHT AND PAYLOAD CONTROL FOR DIRECTIONAL PAYLOADS ON UAVS |
ICAS-98-3.7.2 |
Wong K. C. |
UAVS OVER AUSTRALIA: CAPABILITIES AND OPPORTUNITIES |
ICAS-98-3.7.5 |
Wood L. A. |
DESIGN AND ANALYSIS OF PROPELLERS FOR GENERAL AVIATION AIRCRAFT NOISE REDUCTION |
ICAS-98-5.11.3 |
Woodyatt B. |
PERFORMANCE FLIGHT TESTING OF AN F-111 C AIRCRAFT |
ICAS-98-1.1.1 |
Wu X. H. |
A NEW PROCEDURE FOR SIMULATING ROTOR/STATOR INTERACTION IN TURBOMACHINERY |
ICAS-98-7.4.3 |
Wu X. R. |
PREDICTION OF FATIGUE CRACK GROWTH IN FIBER REINFORCED METAL LAMINATES |
ICAS-98-5.7.5 |
Xie M. |
FINITE ELEMENT MODELING AND EXPERIMENTAL STUDY OF A GAS TURBINE ENGINE BLADE UNDER BIAXIAL LOADING |
ICAS-98-5.1.4 |
Xin D. -D. |
EFFECTS OF USING BI-FLAP-SYSTEM ON THE IMPROVEMENT OF AERODYNAMICS OF A SWEPTBACK WING |
ICAS-98-3.6.2 |
Yamakami J. |
THE MECHANISM OF ACTIVE BOUNDARY LAYER CONTROL USING VORTEX GENERATOR JETS |
ICAS-98-3.4.3 |
Yang C. |
A MATHEMATICAL MODEL OF AFFINE NONLINEAR SYSTEM FOR HELICOPTER FLIGHT DYNAMICS |
ICAS-98-1.4.5 |
Yanova O. V. |
OPTIMIZATION OF SPACE SYSTEM LAUNCHING WITH LIMITATIONS ON FALL ZONES FOR SPENT COMPONENTS |
ICAS-98-1.3.3 |
Yao L. J. |
NUMERICAL SIMULATION OF THE TEMPERATURE FIELD DURING FATIGUE PROCESS |
ICAS-98-7.7.1 |
Yao P. -H. |
CONICAL EULER EQUATIONS' SOLUTION BASED ON THE UNSTRUCTURED GRID AND ITS APPLICATION TO A VORTICAL FLOW OVER A HIGHLY SWEPT DELTA WING |
ICAS-98-7.4.2 |
Ye D. |
NUMERICAL SIMULATION OF THE TEMPERATURE FIELD DURING FATIGUE PROCESS |
ICAS-98-7.7.1 |
Yegorov I. V. |
AEROTHERMODYNAMIC CHARACTERISTICS OF TWO-DIMENSIONAL BLUFF BODIES IN HYPERSONIC VISCOUS FLOWS |
ICAS-98-R.2.1 |
Yegorova M. V. |
AEROTHERMODYNAMIC CHARACTERISTICS OF TWO-DIMENSIONAL BLUFF BODIES IN HYPERSONIC VISCOUS FLOWS |
ICAS-98-R.2.1 |
Yennak Y. N |
ANALYTICAL AND EXPERIMENTAL INVESTIGATIONS OF AN IMPROVED AERODYNAMIC ORBITER CONFIGURATION |
ICAS-98-R.1.2 |
Yong T. |
THE DESIGN OF USER-ORIENTED FATIGUE DATABASE BASED ON CLIENT/SERVER MODEL |
ICAS-98-7.5.3 |
Yu K. H. |
ACTIVE COMBUSTION CONTROL FOR PROPULSION SYSTEMS |
ICAS-98-5.8.2 |
Yuan Z. G. |
CHARACTERISTICS OF MOMENTUM-DOMINATED HYDROCARBON TURBULENT DIFFUSION FLAMES |
ICAS-98-5.8.1 |
Yuceoglu U. |
FREE FLEXURAL VIBRATIONS OF COMPOSITE PLATES OR PANELS STIFFENED BY A CENTRAL OR NON-CENTRAL PLATE STRIP - SOME COMPARISONS |
ICAS-98-R.4.11 |
Yukselen M. A. |
EXPERIMENTAL INVESTIGATION OF A DIFFUSER FOR COOLING AND AIR CONDITIONING SYSTEM |
ICAS-98-7.6.2 |
Zagdanski Z. |
PROBLEMS OF QUALITY OF SIMULATION OF 3 D FLIGHT DYNAMICS OF AIRCRAFT IN FLIGHT SIMULATORS |
ICAS-98-P22 |
Zeghloul A. |
NUMERICAL MODELLING FOR PREDICTING DAMAGE TOLERANCE OF COMPOSITE STRUCTURE |
ICAS-98-5.9.3 |
Zhang F. Z. |
USING THE MEAN LIVES TAKEOFF AND LANDING OF ACTUALLY MEASURING COURSES TO DRAW UP THE AIRCRAFT F-BY-F LOAD SPECTRUM |
ICAS-98-P23 |
Zhuang W. Z. |
NUMERICAL SIMULATION OF FATIGUE CRACK CLOSURE BEHAVIOUR UNDER BIAXIAL LOADING |
ICAS-98-5.7.1 |
Zhuang W. Z. |
PREDICTION OF FATIGUE CRACK GROWTH FROM BOLT HOLES IN A TITANIUM DISC |
ICAS-98-5.2.3 |
Zrnic N. |
COMPARATIVE FORCE AND MOMENT MEASUREMENTS ON FULL AND HALF MODELS IN THE YUGOSLAV T-38 TRISONIC WIND TUNNEL |
ICAS-98-3.6.4 |
Zurek J. |
APPLICATION OF EXPERT METHODS TO RISK ASSESSMENT OF AIR TRANSPORT SYSTEMS |
ICAS-98-R.1.9.2 |