| Title |
Author(s) |
|
|
| CFD and Turbulence |
M LANDAHL |
| |
|
ICAS-VON-KARMAN-LECTURE
|
|
| CFMI and the GEAE - SNECMA Alliance |
L GALLOIS, B ROWE |
| |
|
General lectures
|
|
| Flight Simulation and Digital Flight Controls |
D CHATRENET |
| Advanced Composites Research and Development for Transport Aircraft |
J G DAVIS, JH STARNES |
| The X-31 and Advanced Highly Manoevrable Aircraft |
W HERBST, M R ROBINSON |
| |
|
| |
|
AEROELASTICITY
|
|
| Predicting the Aeroelastic Behaviour of a Wind Tunnel Model using Transonic Small-Disturbance Theory |
R M BENNETT, W A SILVA |
| Transonic Flutter/Divergence Characteristics of Aeroelastically Tailored and Non-Tailored High-Aspect-Ratio Forward Swept Wings |
K ISOGAI |
| Transonic Unsteady Aerodynamic-Influence-Coefficient Method for Aeroelastic Applications |
P C CHEN, D K JAMES, D D LIU |
| Development of a Three-Dimensional Unsteady Transonic Aerodynamics Computer Code for Flutter Analysis |
B H LEE, Y S WONG |
| |
|
MULTIDISCIPLINARY DESIGN INTEGRATION I
|
|
| The Integration of Structural Optimization in the General Design Process for Aircraft |
H GODEL, A LOTZE, O SENSBURG, J SCHWEiGER |
| Conceptual Design of Civil Transport Aircraft by a Numerical Optimization Technique |
D CAVALLI, H T HUYNH, C MICHAUT |
| Applications of the Structural Optimization Program Optsys |
T BRAMA |
| Application of Methods and Tools for Computer-Aided Design in Investigation of Prospects for Civil Aircraft Progress |
V E DENISOV |
| |
|
SLIPSTREAM AND JET INTERFERENCE
|
|
| Measurement of Unsteady Pressures and Forces on an Engine and a Wing/Engine Combination including Jet Simulation |
H TRIEBSTEIN, G SCHEWE, S VOGEL, H ZINGEL |
| Ground-Vortex Formation with Twin Jets and Moving Ground Plane |
D BRAY, K KNOWLES |
| Experimental Investigation of Low Speed Model Propeller Slipstream Aerodynamic Characteristics Including Flow Field Surveys and Nacelle/Wing Static Pressure Measurements |
I SAMUELSSON |
| Mass Flow Effects on the Low Speed Characteristics of an Advanced Combat Aircraft |
A FERRETTI, A GATTI |
| |
|
AEROACOUSTIC DEVELOPMENTS AND ADVANCED PROPELLERS
|
|
| Recent Wind Tunnel Testing Experience of Contra-Rotating Propellers |
A E HARRIS, O POZNIAK, P RENDER, M WOOD |
| Aeroacoustics of Advanced Propellers |
J F GROENEWEG |
| Increased Noise Emission of Propellers and Propfans due to Pusher Installation |
Th LOLGEN, G NEUWERTH, R STAUFENBIEL |
| Reducing Flyover Noise of Propeller-Driven Aeroplanes by Superposition of Propeller and Exhaust Noise |
M KALLERGIS |
| |
|
SIMULATION TECHNOLOGY AND HUMAN FACTORS
|
|
| The NOE Flights and their Effect Upon a Pilot |
R WITKOWSKI |
| Hermes Pilot Training Facility |
F BOUCKAERT |
| Military Aircrew Head Support System |
R DEAKIN |
| The Influence of Aircraft Cabin Configuration on Passenger Evacuation Behaviour |
C MARRISON, H MUIR |
| |
|
BOUNDARY LAYER TESTING
|
|
| The Wind Tunnel as a Tool for Laminar Flow Research |
A ELSENAAR |
| Flight Investigations of Tollmien-Schlichting Waves on an Aircraft Wing |
K H HORSTMANN. S J MILEY, G REDEKER |
| Turbulence Measurements using Silicon Based Sensors |
B JOHANSSON, L LOFDAHL, G STEMME |
| Concepts and Results for Laminar Flow Research in Wind Tunnel and Flight Experiments |
W NITSCHE, J SZODRUCH |
| |
|
AEROELASTICITY II
|
|
| Structural Optimization of Aircraft Practice and Trends |
C PETIAU |
| Supersonic Flutter of Composite Skew Panels |
C SURACE, G SURACE |
| The Aerel Flutter Prediction System |
V J STARK |
| |
|
SENSORS AND SUBSYSTEMS
|
|
| NASA Programs in Advanced Sensors and Measurement Technology for Aeronautical Applications |
B A CONWAY |
| Modern Oxygen and Anti-G Protection for the Pilot of Advanced Fighter Aircraft SAAB JAS 39 |
R BEAUSSANT |
| Fiberoptic Air Data System |
P M DIWAKAR, L C MANOHARAN, S MUTHUVEL, K SESHADHI |
| |
|
HIGH ALPHA, VORTEX FLOWS
|
|
| Three Dimensional Dynamic and Static Stability of Vortex Systems and their Observability and Controllability |
Z RUSAK, A SEGINER |
| Formation of Tip Vortices and Vortex Wake Alleviation by Tip Devices |
R STAUFENBIEL, T VITTING |
| Active Control Experimental Investigation about Aerodynamic Characteristics at High Incidence |
Y YONGNIAN, Y XINZHI, W ZONGDONG, L JIANGYING |
| |
|
AEROACOUSTIC DEVELOPMENTS AND ADVANCED PROPELLERS II
|
|
| Rotor Loads Computation using Singularity Methods and Application to the Noise Production |
P GNEMMI, J HAERTIG, M SCHAFFAR |
| Effects of Shear Flow on Sound Transmission Across Boundary Layers |
L M CAMPOS, P G SERRAO |
| A Navier-Stokes Calculation of the Flow Passing Through a Cascade with Tip Clearance |
O NOZAKI, A TAMURA, T WATANABE |
| |
|
ROTORCRAFT
|
|
| Aerodynamic Design of a Tilt Rotor Blade |
B BENOIT, J M BOUSQUET |
| Rotorcraft Blade/Vortex Interaction Noise: Its Generation, Radiation, and Control |
T F BROOKS, R M MARTIN, J S PREISSER |
| Aeroelastic Stability of Composite Bearingless Rotor Blades |
X MING, W SHI-CUN |
| |
|
NEW TEST FACILITIES
|
|
| Status of Adaptive Wall Technology for Minimization of Wind Tunnel Boundary Interferences |
S W WOLF |
| Performance of a New Roll-In Roll-Out Transonic Test Section of the NAE 1.5m x 1.5m Blowdown Wind Tunnel |
D BROWN, L H OHMAN |
| The FFA T1500 Injection Driven Transonic Wind Tunnel |
L TORNGREN |
| |
|
AEROELASTICITY III
|
|
| Control Law Synthesis and Wind Tunnel Test of Gust Load Alleviation for a Transport-Type Aircraft |
Y ANDO, K FUJI I, M HASHIDATE, H MATSUSHITA, Y MIYAZAWA, T UEDA |
| Design, Implementation, Simulation and Testing of a Digital Flutter Suppression Systems for the Active Flexible Wing Wind Tunnel Model |
C J BUTTRILL, S R COLE, S T HOADLEY, J A HOUCK, V MUKHOPADHYAY, B PERRY |
| Whirl-Flutter Suppression in Advanced Turboprops and Propfans by Active Control Techniques |
F NITZSCHE |
| Identification of Dynamic Response, Simulation and Design of a Highly Non-Linear Digital Load Alleviation System for a Modern Transport Aircraft |
G BEUCK, H ELLGOTH, G ROLLWAGEN |
| |
|
MULTIDISCIPLINARY DESIGN INTEGRATION II
|
|
| Multidisciplinary Optimization in Aircraft Design |
D L KIRKPATRICK, J S SMITH |
| Optimization of Aircraft Configurations in a Multidisciplinary Environment |
F ABDI, T LOGAN, J SOBIESZCZANSKI-SOBIESKI |
| Sensitivity Analysis of a Wing Aeroelastic Response |
J-F BARTHELEMY, R K KAPANIA |
| Application of Advanced Multidisciplinary Analysis and Optimization Methods to Vehicle Design Synthesis |
R D CONSOLI, J SOBIEZCZANSKI-SOBIESKI |
| |
|
HIGH ALPHA FLOW OVER WINGS
|
|
| Numerical Simulation of High-Incidence Flow Over the F-18 Aircraft |
N CHADERJIAN, R CUMMINGS, Y M RIZK, L B SCHIFF |
| Force Measurements and Visualisation on a 60-Degree Delta Wing in Oscillatory and Stepwise Pitching Motion |
P TORLUND |
| Numerical Simulation of the Vortical Flow over a Delta Wing at Subsonic and Transonic Speeds |
H W HOEIJMAKERS, J JACOBS, J VAN DEN BERG |
| Comparison of Experimental Results with the Non-Linear Vortex Lattice Method Calculations for Various Wing-Canard Configurations |
D ALMOSNINO, B MELAMED, J ROM |
| |
|
BUCKLING AND POST-BUCKLING
|
|
| Theoretical and Experimental Investigation of Stringer Peeling Effects at Stiffened Shearloaded Composite Panels in the Postbuckling Range |
D HACHENBERG, H KOSSIRA |
| Buckling of Composite Cylindrical Shells in Compression and Torsion |
V GIAVOTTO |
| Buckling of Composite Plates and Columns under Axial Impact |
H ABRAMOVICH, K JORDE, H ROEHRLE, J SINGER, T WELLER |
| Behaviour of a Local Delamination under Compressive Load |
D GUEDRA-DEGEORGES, S MAISON |
| |
|
INLETS AND NOZZLES
|
|
| Prediction of Inlet Drag for Conceptual Aircraft Design |
E BROWN, P MALAN |
| Engine Inlet Ice Protection and Compressor Changes Made to Resist Ice |
L W BLAIR, R L MILLER, D J TAPPARO |
| Control of Flow Separation and Mixing by Aerodynamic Excitation |
J M ABBOTT, E J RICE |
| Some Aspects on the Joint GE/Volvo Development of the F404/RM12 Augmentor |
J C MAYER, S OLOVSSON, B SJOBLOM |
| |
|
SIMULATION AND FLIGHT TEST
|
|
| In-Flight Simulator for Evaluation of Perspective Control Concepts of the Transport Airplane |
S BORIS V ROGOZIN |
| Approach Accuracy of Commuter Aircraft under Variable Wind Conditions |
W KINDEL |
| On the Development of the BAFR (Basic Aircraft for Flight Research) in Portugal |
J R AZIN HE IRA, L M CAMPOS |
| Test and Verification Philosophy in Development of the Anti-Armour Projectile STRIX |
T JOHANSSON |
| |
|
AEROELASTIC RESPONSE
|
|
| Harmonization of US and European Gust Criteria for Transport Airplanes |
T J BARNES |
| Static Aeroelastic Analysis of Composite Wing |
C S HONG, S H KIM, I LEE, H MIURA |
| Non-Linear Flutter Analysis of Wings at High Angle of Attack |
Z Y YE, L C ZHAO |
| Modelling and Model Simplification of Aeroelastic Vehicles |
C S BUTTRILL, D K SCHMIDT, M R WASZAK |
| |
|
SYSTEMS ARCHITECTURE AND INTEGRATION
|
|
| New Avionics Architecture Concept for Commercial Aircraft |
D GRAVES, H SUBRA, M PAQUIER |
| Integration - The Basis of the Integrated Approach to the Passenger Aircraft Control Systems Design |
S P KRJUKOV, V SMIRNOV |
| A Systems Approach to Avionic Multiprocessing Architectures |
J D SEALS |
| Three Real-Time Architectures: A Study using Reward Models |
J A SJOGREN, R M SMITH |
| |
|
UNSTEADY AERODYNAMICS
|
|
| A Review of Scale Effects in Unsteady Aerodynamics |
D G MABEY |
| Observations of Dynamic Stall Phenomena on an Oscillating Airfoil with Shear-Stress-Sensitive Liquid Crystal Coatings |
D C REDA |
| Experiments on the Establishment of Fully Attached Aerofoil Flow from the Fully Stalled Condition during Ramp-Down Motions |
R A GALBRAITH, A J NIVEN |
| The Effect of Periodical Flap Motion on Boundary Layer and Wake |
N ELDEM |
| |
|
FATIGUE AND FRACTURE MECHANICS I
|
|
| Cyclic Shear Buckling of Thin-Walled Aluminium Panels |
P HORST, H KOSSIRA |
| A Model for Predicting Damage Induced Fatigue Life of Laminated Composite Structural Components |
D H ALLEN, I T GEORGIOU, C E HARRIS, D C LO |
| Computer Aided Fatigue and Damage Tolerance Sizing |
H ANSELL |
| Monitoring Load Experience of Individual Aircraft |
J B DE JONGE |
| |
|
PROPULSION INTEGRATION
|
|
| Applications of CFD Technology to the Design of Aircraft Propulsion Systems |
L J HEBERT, R E PONSONBY |
| STOVL Aircraft Propulsion Integration |
J L BENSON, Y T CHIN, G HERSTINE, D RAYMER |
| A Study of Propeller-Wing-Body Interference for a Low Speed Twin- Engined Pusher Configuration |
M G MAUNSELL |
| A Propeller Slipstream Model in Subsonic Linearized Potential Flow |
P LOTSTEDT |
| |
|
CFD CONFIGURATIONS I
|
|
| Flow Simulation around a Realistic Fighter Airplane Configuration |
T BERGLIND |
| A Transonic/Supersonic CFD Analysis of a Generic Fighter |
A M GOODSELL, M D MADSON, J E MELTON |
| Aerodynamic Calculation of Complex Three-Dimensional Configurations |
R LARGUIER, F ROGGERO |
| Applications of a Multizone Euler/Navier-Stokes Aerodynamic Method To Aircraft Configurations |
C R OLLING, P RAJ, S W SINGER |
| |
|
TRAJECTORY OPTIMIZATION AND GUIDANCE
|
|
| Near-Optimal Guidance Trajectories for Coplanar, Aeroassisted Orbital Transfer |
A MIELE, T WANG |
| Optimal Re-Entry Trajectories Yielding Reduced Absorbed Heat and Extended Cross Range |
M K HORN |
| A Missile Control System Based on A1 Ideas |
E SKARMAN |
| |
|
AVIONICS
|
|
| Avionics Systems Functional Analysis and Specification |
P SCHIRLE |
| On Calculation of Predicted Tracer Line using FIFO Structure |
C GONG, P ZHU |
| Validation of Advanced Safety Enhancements for F-16 Terrain Following |
J G BLAYLOCK. B HICKS, D SWIHART, W URSCHEL.PBOOSE |
| |
|
HIGH ALPHA DYNAMICS
|
|
| Prediction of High Alpha Vehicle Dynamics |
L E ERICSSON |
| Prediction of Vortex Shedding from Forebodies with Chines |
D J LESIEUTRE, M R MENDENHALL |
| Computation of Asymmetric Vortex-Flow around Circular Cones using Navier-Stokes Equations |
H A KANDIL, O A KANDIL, C H LIU, T WONG |
| |
|
FATIGUE AND FRACTURE MECHANICS II
|
|
| Fatigue Crack Propagation in Aerospace Aluminium Alloys |
D L DICUS, R P GANGLOFF, R S PIASCIK, J C NEWMAN |
| Damage Tolerance Analysis and Testing of the Fighter Aircraft 37 Viggen |
A BLOM, P BOMAN, M OLSSON, B PALMBERG |
| High Cycle Multiaxial Fatigue |
D L McDIARMID |
| |
|
EXPERIMENTAL TECHNIQUES I
|
|
| Existing and New Hypersonic Facilities Required for Hermes Spacecraft Testing |
G DE RICHEMONT |
| A Flight Experiment to Measure Rarefied-Flow Aerodynamics |
R C BLANCHARD |
| Unsteady Flows Around an Oscillating Flat Model using an Embodied Technique of Fibre Optics Laser Velocimeter |
J BELLEUDY, D FAVIER, C MARESCA |
| |
|
STRUCTURAL DYNAMICS AND IMPACT
|
|
| Vibration Analysis of Stiffened Cylindrical Thin Shells |
M C DOKMECI, Z MECITOGLU |
| Effect of Low Velocity Impact Damage on the Buckling Behaviour of Composite Panels |
G GAETANI, C GRASSI, G ROMEO |
| Summary of a Study to Determine Low-Velocity Impact Damage and Residual Strength for a Thick Graphite/Epoxy Motor Case |
C POE |
| A New Method for the Dynamic Analysis of Large Structures |
R BARBONI, P GAUDENZI, A MANNINI, P SANTINI |
| |
|
COMPUTATIONAL AIDS FOR TRANSPORT AIRCRAFT
|
|
| A Computational and Experimental Analysis of Joined-Wing Aerodynamics |
H HASHIMOTO, N HIROSE, M ISHIKAWA, T OHNUKI |
| Design and Validation of Advanced Transonic Wings using CFD and Very High Reynolds Number Wind Tunnel Testing |
M I GOLDHAMMER, F W STEINLE |
| Machine Part Supplier Use of Catia Data on Non-Catia CAD/CAM Systems |
W A CREEL |
| Some New Developments on the Aircraft Design and Analysis System (ADAS) |
C BIL, J MIDDEL |
| |
|
DRAG REDUCTION
|
|
| ONERA Activities on Drag Reduction |
J RENEAUX, J THIBERT, V SCHMITT |
| Analysis of Crescent Wings using a Subsonic Panel Method |
C W BURKETT |
| Supersonic Laminar Flow Control on Commercial Transports |
F S COLLIER, M C FISCHER, W PFENNINGER, R D WAGNER |
| Laminar Flow Experiments with a Large Half Model in Transonic Flow |
R HENKE, F X MUNCH |
| |
|
HIGH TEMPERATURE MATERIALS AND METALLIC ALLOYS
|
|
| Silicon Carbide Fibre-Reinforced Glass-Ceramics Matrix Composites: A High Temperature Material for High-Performance Application |
M PARLIER, M H RITTI, J F STOHR, S VIGNESOULT |
| Intermetallic Compounds for High Temperature Use in Aerospace Industry |
P COSTA, T KHAN, P VEYSSIERE, SNAKA |
| Characterization and Modelling of the Anisotropic Mechanical Behaviour of Nickel-Based Single Crystal Superalloys for Turbine Blades |
P CARON, T KHAN, P POUBANNE |
| High-Strength Structural Steels for Landing Gear Components |
A F PETRAKOV, N POKROVSKAYA, O REVYAKINA |
| |
|
AIRCRAFT CONTROL
|
|
| Robust Control System Design with Multiple Model Approach and its Application to Flight Control System |
Y MIYAZAWA |
| Gaming in Fuselage Aiming |
B JARMARK |
| Development of Lateral Control on Aircraft Operating at Very High Angles of Attack |
N J WOOD |
| An Algorithm for Decoupling Vertical/Horizontal Motions of Non-Symmetric Rolling Aircraft |
E M BELO, P W FORTESCUE |
| |
|
CFD CONFIGURATIONS II
|
|
| Numerical Investigation of the Origin of Vortex Asymmetry of Flows over Bodies at Large Angle of Attack |
D DEGANI |
| Application of a Multiblock CFD System to Obtaining Flowfield Predictions about Wing Body Pylon Store Configuration |
A J BAXENDALE |
| Blunt Trailing Edge Analysis of Supercritical Airfoils by a Navier- Stokes Code |
N HIROSE, N KAMIYA |
| Laminar Supersonic Flow Calculations around Spheres and Cylinders |
A ALUND, Y C SEDIN |
| |
|
VIBRATION, IMPACT AND CRASH RESISTANCE
|
|
| Behaviour of Composite/Metal Aircraft Stuctural Elements and Components under Crash-Type Loads - What are They Telling us? |
R L BOITNOTT, H D CARDEN, E L FASANELLA |
| Analysis of the Dynamic Behaviour of Aircraft Structures During Crash Impacts |
L NERI, G WITTLIN |
| Hypervelocity Impact Testing of Non-Metallic Materials |
W P SCHONBERG |
| Free Vibrations of Thin-Walled Composite Semicircular Graphite- Expoxy Frames |
H D CARDEN, A K NOOR, J M PETERS |
| |
|
TRANSPORT AIRCRAFT DESIGN INTEGRATION
|
|
| Aerodynamic Design for a New Regional Aircraft |
E GREFF |
| Quiet STOL Research Aircraft - Development and Flight Test |
A SUKA, Y HAYASHI, M MORI, N TAKASAKI, T TSUJIMOTO |
| Aspects of Theoretical and Experimental Investigations on Airframe/Engine Integration Problems |
W BAUMERT ETAL |
| Engine Installation Design for Subsonic Transport Aircraft |
J MIRAT. R PERIN |
| |
|
SUBSONIC WINGS AND AIRFOILS
|
|
| Jet Trainer Aerofoil Selection |
J BENETKA, M KLADRUBSKY, Z PERNICA |
| The Lift and Pitching Moment Characteristics of an Airfoil in Isolated and Tandem Cases |
M A YUKSELEN |
| An Investigation into the Flow at the Junction Between a Flat Plate and an Aerofoil |
D J ABDULRAZAK, D R PHILPOTT |
| Transonic Wing Design for Transport Aircraft |
J HUA Z Y ZHANG |
| |
|
HYPERSONIC PROPULSION
|
|
| Air Breathing Combined Engines for Space Launchers |
A LARDELLIER, P RAMETTE, D SCHERRER |
| Auxiliary Propulsion for Hypersonic Vehicles |
A GANY, Y M TIMNAT |
| Analysis and Optimization of Scramjet Inlet Performance |
R McGREGOR, S MOLDER |
| Compact Ramjet Combustion Instability - An Overview |
G D ROY |
| |
|
AIRCRAFT CONTROL II
|
|
| Tools and Methods used for Certification of the Fokker 100 Automatic Landing System Performance |
A MULDER, H C VAN DE HULST |
| An Analysis of Reduced Order System for Airplane Gust Alleviation |
J CHANG |
| Integrated Structural Optimization in the Preliminary Aircraft Design |
G BINDOLINO, M LANZ, P MANTEGAZZA, S RICCI |
| Load Alleviation and Ride Smoothing Investigations using ATTAS |
V HAHN, R KÖNIG |
| |
|
CFD CONFIGURATIONS III
|
|
| Prediction of Inviscid Supersonic/Hypersonic Aircraft Flowfields |
D STOOKESBERRY, A VERHOFF |
| Numerical Analysis of Viscous Hypersonic Flow Past a Generic Forebody |
M A SCHMATZ, K M WANIE |
| Large-Scale Numerical Aerodynamic Simulations for Complete Aircraft Configurations |
S TAKANASHI |
| Transport Aircraft Aerodynamic Improvement by Numerical Optimization |
D DESTARAC, J RENEAUX |
| |
|
CERTIFICATION AND STRUCTURAL TESTING
|
|
| Certification of Large airplane Composite Structures, Recent Progress and New Trends in Compliance Philosophy |
J ROUCHON |
| Early In-Flight Detection of Fatigue Cracks in Aero-Engine Compressor and Turbine Blades with Vibroacoustic and Descrete- Phase Methods |
H DABROWSKI, R KUDELSKI, J LEWITOWICZ, R SZCZEPANIK |
| A Software-Based Ground Vibration Testing System |
R J McKINNELL, D WILSON |
| |
|
AIR TRAFFIC CONTROL
|
|
| Strategic Options for Future Air Traffic Systems |
S A MAGILL |
| Four-Dimensional Fuel-Optimal Flights into and out of the Terminal Area |
H G VISSER |
| Extended Range Operations of Two and Three Turbofan Engined Airplanes |
R MARTINEZ-VAL, E PEREZ |
| |
|
EXPERIMENTAL TECHNIQUES II
|
|
| Effects of Reynolds Number, Mach Number and Sting Geometry on Rotary Balance Measurements |
C O'LEARY, B WEIR |
| In-Flight Pressure Distribution Measurements; Instrumentation, Data Handling and Comparison with Wind Tunnel Data |
H KANNEMANS, D F VOLKERS |
| Development of a Measurement Technique for Damping Derivatives in Pitch |
A CAVALLARI, G GUGLIERI, F B QUAGLIOTTI |
| |
|
HIGH TEMPERATURE STRUCTURES
|
|
| Analysis of Precision Sandwich Structures under Thermal Loading |
W ELSPASS, M FLEMMING |
| Advanced Fabrication Technology for High Speed Aircraft Structures |
T BALES, R BIRD, E HOFFMAN |
| An Integrated Thermoelastic Analysis for Periodically Loaded Space Structures |
D GIVOLI, O RAND |
| |
|
SAILPLANES AND COMMUTER AIRCRAFT
|
|
| New Aircraft Platforms for Earth System Science: An Opportunity for the 1990s |
J S LANGFORD |
| The Design and Flight Testing of a Long Endurance RPV |
T KWA, S SIDDIQI |
| Dornier 328 - The Regional Airliner for the Nineties |
R BIRRENBACH, W SCHMIDT |
| |
|
CFD DEVELOPMENTS
|
|
| Computing Aerodynamics on Parallel Computers |
S C GUPTA |
| Parallel Implementation of an Explict Finite Volume Euler Solver on an Array of Transputers |
S TURNOCK |
| Recent Developments in CFD at ARA |
A J BOCCI |
| |
|
FLIGHT SAFETY
|
|
| Airborne Collision Avoidance System - The UK Experience |
R M ABLETT |
| Optimal Filtering of Sensor Signals for Take-Off Performance Monitors (TOPM) |
R KHATWA |
| Reducing Wind Shear Risk through Airborne Systems Technology |
R BOWLES |
| Structure and Method of the Expert System for Sensor Failure Detection of Aircraft |
Z SHI |
| |
|
SUPERSONIC AND HYPERSONIC AIRCRAFT
|
|
| What Speed for a Future High-Speed Transportation System? |
P POISSON-QUINTON |
| Design Aspects of Long Range Supersonic LFC Airplanes with Highly Swept Wings |
W PFENNINGER, C S VEMURU |
| Integrated Fluid-Thermal-Structural Analysis using Adaptive Unstructured Meshes |
P DECHAUMPHAI |
| Project Designs of Alternative Versions of the SL-86 2-Stage Horizontal Take-Off Space Launcher |
J P FIELDING |
| |
|
SUPERSONIC WINGS AND AIRFOILS
|
|
| Flow Features of Highly-Swept Wings at Subsonic and Supersonic Speeds |
P R AS HILL, C J BETTS, J L FULKER, M J SIMMONS |
| Aerodynamic Analysis of the Flow Characteristic of a Delta-Canard Configuration |
A FERRETTI, A SALVATORE |
| Investigations into the Flow Behind Castellated Blunt Trailing Edge Aerofoils in Supersonic Flow |
S L GAI, E C MAGI, A PRYTZ |
| Some Design Considerations and Prospects of Applying Leading- Edge Vortex Flaps to Combat Aircraft Wings |
R K NANGIA, G E LOCKLEY |
| |
|
STRUCTURAL STRENGTH AND RESPONSE ANALYSIS
|
|
| Large Deflection Nonlinear Response of Laminated Composite Plates Subjected to Static, Thermal and Acoustic Loads |
J E LOCKE |
| Accurate and Reliable Determination of Edge and Vertex Stress Intensity Factors in Three-Dimensional Elastomechanics |
B ANDERSSON, I BABUSKA, U FALK |
| Development of Structural Strength Finite-Element Analysis Techniques |
V D CHUBAN |
| Postbuckling of Long Thick Plates in Compression Including Higher Order Transverse Shearing Effects |
L LIBRESCU, M STEIN, P D SYDOW |
| |
|
AIRCRAFT MANOEUVRABILITY AND HANDLING QUALITIES
|
|
| Modelling and Classification of Helicopter Combat Monoeuvres |
R BRADLEY, D G THOMSON |
| Longitudinal Handling Improvements of Pilatus PC-9 Advanced Turbo Trainer |
A CERVIA, A TURI |
| Aerodynamics, Performance and Control of Airplanes in Formation Flight |
M BEUKENBERG, D HUMMEL |
| Status of Agility Research at McDonnell Aircraft Company and Major Findings and Conclusions to Date |
M H DRAJESKE, D R RILEY |
| |
|
CFD DEVELOPMENTS II
|
|
| Aerodynamic Design Via Optimization |
K D LEE.SEYI |
| Convergence Acceleration and Wave Drag Determination inTransonic Airfoil Calculations |
S V LYAPUNOV |
| Development and Validation of Characteristic Boundary Conditions for Cell-Centered Euler Methods |
J W BOERSTOEL, J I VAN DEN BERG |
| Development of Unstructured Grid Methods for Steady and Unsteady Aerodynamic Analysis |
J T BATINA |
| |
|
AIRWORTHINESS, RELIABILITY AND MAINTENANCE
|
|
| Continuing Airworthiness - Requirements Substantiation |
F C FICKEISEN |
| Diagnosis on New Civil Airplanes - Economic Aspects |
P CAMUS |
| Composite Repair - An Airlines Point of View |
E MOYSON |
| An Integrated Research on Composite Helicopter Crashworthiness |
V GIAVOTTO |
| |
|
MILITARY AIRCRAFT
|
|
| Military Trainer Aircraft - Turboprop or Jet? |
E A P BURDAK, O MASEFIELD |
| Advanced Aircraft Analysis: A User-Friendly Approach to Preliminary Aircraft Design |
J ROSKAM ,S M MALAEK , W ANEMAAT |
| Design and Flight Test on High AOA/Spin Characteristics of XT-4 Intermediate Jet Trainer |
F HAYASHI, T ICHIHASHI, H KOMAKI, N MORITA, N TODA, N UDAGAWA |
| Adapting Existing Commercial Aircraft Designs to Meet Existing and Future Military Aircraft Requirements |
L LADDIE COBURN |
| |
|
HYPERSONIC AEROTHERMODYNAMICS
|
|
| Experimental Study on Drag Reduction of Hypersonic Transport Configuration |
Y AIHARA, K HOZUMI, E MORISHITA, S NOMURA, T OKUNUKI |
| The Effects of Different Gas Models on the Hypersonic Viscous Flow Over Re-Entry Vehicles |
S JIANWEI, Q ZHANGHUA |
| Compression Corner Shock Wave Boundary Layer Interactions at Mach 14 |
G SIMEONIDES, J F WENDT |
| Numerical Experiments using Navier Stokes Codes for Generalised Hypersonic Shapes |
N QIN, B RICHARDS, Z WANG |
| |
|
PROPERTIES AND FABRICATION PROBLEMS OF COMPOSITE MATERIALS
|
|
| Analytical and Experimental Studies on Creep Behaviour of Polymeric Matrix Composites |
I H HWANG, K Y LIN |
| Viscoelastic Modelling of Continuous Carbon Fibre Reinforced Thermoplastics |
C BAXENVANAKIS, G PAPANICOLAOU |
| The Effect of Electric Properties of Advanced Composites on the Design for Modern Aircraft |
P HSU |
| Gel Time Measurements on Carbon Fibre/Epoxy Resin Prepregs |
J ALARY, S LAZCANO, A RODRIGUEZ, A SANCHEZ, J SANCHEZ |
| |
|
NON-LINEAR FLIGHT DYNAMICS
|
|
| Nonlinear Modelling in Airborne Simulations |
J M BAUSCHAT |
| Post Stall Characteristics of Highly Augmented Fighter Aircraft |
M MEDINA, M SHAHAF |
| A Study of Wing Rock |
H GAO, Z WANG, S ZHANG |
| Bifurcation Theory in Flight Mechanics - An Application to a Real Combat Aircraft |
P GUICHETEAU |
| |
|
CFD DEVELOPMENTS III
|
|
| Improved Mesh Sequencing Method for the Accelerated Solution of the Compressible Euler and Navier-Stokes Equations |
D DRIKAKIS, S TSANGARIS |
| Numerical Simulation of High Speed Compressible Flows with Upwind Schemes on Adapted Unstructured Grids |
L FORMAGGIA, V SELMIN |
| A Multigrid LU Factorization Scheme for the Thin-Layer Navier-Stokes Equations |
J HOFFREN, S LAINE, T SIIKONEN |
| Methods to Enhance the Accuracy of Finite Volume Schemes |
T SCHONFELD, P WILDE |
| |
|
MATHEMATICAL MODELLING AND APPLICATIONS
|
|
| Mathematical Modelling of Optimal Passive Control of Rotor Head Vibrations |
J JANKOVIC |
| Analysis of Methods for Modelling Real Flight Situation |
J ROHACS |
| Three Dimensional Transonic Full Potential Solution by an Integral Equation Method |
J P AGARWAL, N L ARORA |
| |
|
| |
|
Reserve Papers
|
|
| Controlling the Leading-Edge Vortex on the Vortex Flap Using Mass Injection |
T HSING, Y QIN, F ZHUANG |
| Applicability of Euler Analysis to Prop-Fan Aerodynamic Design |
Y KAWAKAMI, M KOBAYAKAWA, F METZGER, R TAKAKI |
| Reynolds Stress Measurements on a Prolate Spheroid at Incidence |
G IUSO, M S OGGIANO, M ONORATO, S DE PONTE |
| A Concept of Stall Warning System |
J F ELASKAR |
| Finite Element Application to Interior Noise Prediction in Aircraft Fuselage |
S HAEUSLER, C WENIGWIESER |
| Subsonic Steady, Unsteady Aerodynamic Calculation for Wings at High Angle of Attack |
Y YANG, Z YE, L ZHAO |
| Modern Developments in Shear Flow Control with Swiri |
S FAROKHI, E J RICE, R TAGHAVI |
| Flight Test Validation of the Operational Loads Monitoring System (OLMS) |
Y LADDA, M C SCHMUCKER |
| Dynamic Response of Anisotropic Composite Panels to Time- Dependent External Excitations |
L LIBRESCU, A NOSIER |
| Viscous Supersonic Flow Past a Wedge-Shaped Body |
Z DZYGADLO, S WRZESIEN |
| Two-Step Method for the Calculation of Wall Interferences in Slotted Test Sections |
J AMECKE |
| Computer-Aided Conceptual Aircraft Configuration Development by an Integrated Optimization Approach |
W FENSKE, C HABERLAND, O KRANZ, R STOER |
| Hypersonic Flow Fields around Hermes Computed by Euler Codes |
B ARLINGER, B WINZELL |
| The Reduction of Rigid-Body Response on Sting Supported Models at High Angies of Incidence |
D G MABEY, C R PYNE, B L WELSH |
| Design Optimization of Natural Laminar Flow Fuselages in Compressible Flow |
S DODBELE |
| The Analysis of Three Icing Flights with Various Ice Accretion Stuctures when Reaching Icing Degree Severe |
H E HOFFMANN |
| The Design of Intercontinental Supersonic Transport Aircraft of Second Generation by Using Global Optimization Techniques |
A NASTASE |
| An Integrated Approach to Design for Reliability Maintainability and Mission Readiness of Combat Aircraft |
J P FIELDING |
| Commercial Aircraft Composite Thrust Reverser Blocker Door Manufactured Using the Resin Transfer Molding Technique |
K KRAFT |
| Bifurcation Methods - A Practical Methodology for Implementation by Flight Dynamicists |
M H LOWENBERG |
| High Resolution Upwind Solutions of the Incompressible Navier- Stokes Equations |
G DEGREZ, A TAHI |
| A New Theory of Turbulence Based on the Concept of Fractal Analysis |
G GAO, W CHOW |
| Non-Linear Mathematical, Thermal Models of Gas Turbine Engines and their Application in Operation |
I SANTA |
| |
|
| |
|
| In Memoriam |
|
| |
|
| The International Council of the Aeronautical Sciences |
|
| |
|
| ICAS Program Committee |
|
| ICAS Member Associations |
|
| ICAS Associate Members |
|
