Title 
Author(s) 


CFD and Turbulence 
M LANDAHL 


ICASVONKARMANLECTURE


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 X31 and Advanced Highly Manoevrable Aircraft 
W HERBST, M R ROBINSON 




AEROELASTICITY


Predicting the Aeroelastic Behaviour of a Wind Tunnel Model using Transonic SmallDisturbance Theory 
R M BENNETT, W A SILVA 
Transonic Flutter/Divergence Characteristics of Aeroelastically Tailored and NonTailored HighAspectRatio Forward Swept Wings 
K ISOGAI 
Transonic Unsteady AerodynamicInfluenceCoefficient Method for Aeroelastic Applications 
P C CHEN, D K JAMES, D D LIU 
Development of a ThreeDimensional 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 ComputerAided 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 
GroundVortex 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 ContraRotating 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 PropellerDriven 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 TollmienSchlichting 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 AntiG 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 NavierStokes 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 SHICUN 


NEW TEST FACILITIES


Status of Adaptive Wall Technology for Minimization of Wind Tunnel Boundary Interferences 
S W WOLF 
Performance of a New RollIn RollOut 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 TransportType 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 
WhirlFlutter Suppression in Advanced Turboprops and Propfans by Active Control Techniques 
F NITZSCHE 
Identification of Dynamic Response, Simulation and Design of a Highly NonLinear 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 SOBIESZCZANSKISOBIESKI 
Sensitivity Analysis of a Wing Aeroelastic Response 
JF BARTHELEMY, R K KAPANIA 
Application of Advanced Multidisciplinary Analysis and Optimization Methods to Vehicle Design Synthesis 
R D CONSOLI, J SOBIEZCZANSKISOBIESKI 


HIGH ALPHA FLOW OVER WINGS


Numerical Simulation of HighIncidence Flow Over the F18 Aircraft 
N CHADERJIAN, R CUMMINGS, Y M RIZK, L B SCHIFF 
Force Measurements and Visualisation on a 60Degree 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 NonLinear Vortex Lattice Method Calculations for Various WingCanard Configurations 
D ALMOSNINO, B MELAMED, J ROM 


BUCKLING AND POSTBUCKLING


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 GUEDRADEGEORGES, 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


InFlight 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 AntiArmour 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 
NonLinear 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 RealTime 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 ShearStressSensitive Liquid Crystal Coatings 
D C REDA 
Experiments on the Establishment of Fully Attached Aerofoil Flow from the Fully Stalled Condition during RampDown 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 ThinWalled 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 PropellerWingBody 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 ThreeDimensional Configurations 
R LARGUIER, F ROGGERO 
Applications of a Multizone Euler/NavierStokes Aerodynamic Method To Aircraft Configurations 
C R OLLING, P RAJ, S W SINGER 


TRAJECTORY OPTIMIZATION AND GUIDANCE


NearOptimal Guidance Trajectories for Coplanar, Aeroassisted Orbital Transfer 
A MIELE, T WANG 
Optimal ReEntry 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 F16 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 VortexFlow around Circular Cones using NavierStokes 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 RarefiedFlow 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 LowVelocity 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 JoinedWing 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 NonCatia 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 FibreReinforced GlassCeramics Matrix Composites: A High Temperature Material for HighPerformance 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 NickelBased Single Crystal Superalloys for Turbine Blades 
P CARON, T KHAN, P POUBANNE 
HighStrength 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 NonSymmetric 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 CrashType 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 NonMetallic Materials 
W P SCHONBERG 
Free Vibrations of ThinWalled 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 
LargeScale 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 InFlight Detection of Fatigue Cracks in AeroEngine Compressor and Turbine Blades with Vibroacoustic and Descrete Phase Methods 
H DABROWSKI, R KUDELSKI, J LEWITOWICZ, R SZCZEPANIK 
A SoftwareBased Ground Vibration Testing System 
R J McKINNELL, D WILSON 


AIR TRAFFIC CONTROL


Strategic Options for Future Air Traffic Systems 
S A MAGILL 
FourDimensional FuelOptimal Flights into and out of the Terminal Area 
H G VISSER 
Extended Range Operations of Two and Three Turbofan Engined Airplanes 
R MARTINEZVAL, E PEREZ 


EXPERIMENTAL TECHNIQUES II


Effects of Reynolds Number, Mach Number and Sting Geometry on Rotary Balance Measurements 
C O'LEARY, B WEIR 
InFlight 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 TakeOff 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 HighSpeed Transportation System? 
P POISSONQUINTON 
Design Aspects of Long Range Supersonic LFC Airplanes with Highly Swept Wings 
W PFENNINGER, C S VEMURU 
Integrated FluidThermalStructural Analysis using Adaptive Unstructured Meshes 
P DECHAUMPHAI 
Project Designs of Alternative Versions of the SL86 2Stage Horizontal TakeOff Space Launcher 
J P FIELDING 


SUPERSONIC WINGS AND AIRFOILS


Flow Features of HighlySwept 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 DeltaCanard 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 ThreeDimensional Elastomechanics 
B ANDERSSON, I BABUSKA, U FALK 
Development of Structural Strength FiniteElement 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 PC9 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 CellCentered 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 UserFriendly Approach to Preliminary Aircraft Design 
J ROSKAM ,S M MALAEK , W ANEMAAT 
Design and Flight Test on High AOA/Spin Characteristics of XT4 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 ReEntry 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 


NONLINEAR 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 NavierStokes 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 ThinLayer NavierStokes 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 LeadingEdge Vortex on the Vortex Flap Using Mass Injection 
T HSING, Y QIN, F ZHUANG 
Applicability of Euler Analysis to PropFan 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 WedgeShaped Body 
Z DZYGADLO, S WRZESIEN 
TwoStep Method for the Calculation of Wall Interferences in Slotted Test Sections 
J AMECKE 
ComputerAided 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 RigidBody 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 
NonLinear Mathematical, Thermal Models of Gas Turbine Engines and their Application in Operation 
I SANTA 




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