ICAS 1990 Stockholm

Cover
Preface
Table of contents

 
Title Author(s)

THE DANIEL AND FLORENCE GUGGENHEIM MEMORIAL LECTURE

 
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
   
   
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