COMPLETE AUTHOR LIST HYPERLINKED TO ABSTRACTS

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