| Title |
Author(s) |
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| The Aerodynamic Potential of Anti-Sound |
J.E. FFOWCS WILLIAMS |
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ICAS-VON-KARMAN-LECTURE
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| The 767 Program: A "First" in International Cooperation |
F. CERETI |
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General lectures
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| Aeroelasticity Today and Tomorrow |
G. COUPRY |
| Future Trends in Propulsion |
S.C. MILLER, H.W. BENNETT |
| Atmospheric Disturbances Affecting Safety of Flight |
A. R. MULALLY , C. R. HIGGINS |
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History Lecture
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| The Race for Speed from the Beginning of Aviation to the Present Day |
P. LISSARAGUE, P. LECOMTE |
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Airfoil Design
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| Thick Supercritical Airfoils with Low Drag and NLF Capability |
B. EGGLESTON, D.J. JONES R.J.D. POOLE, M. KHALID |
| Design of a Supercritical Airfoil |
Z.Y. ZHANG, X.T. YANG B. LASCHKA |
| Investigations on High Reynolds Number Laminar Flow Airfoils |
G. REDEKER, K. H. HORSTMANN, H. KOSTER, A. QUAST |
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Transport Aircraft
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| Optimization of Jetstream in the Commuter Environment |
J. LARROUCAU |
| Influence of EFCS-Control Laws on Structural Design of Modern Transport Aircraft |
M. BESCH, C.L. TANCK |
| 747 Modernization |
R.A. DAVIS |
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CAD - CAM
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| Applications of Computer-Aided Engineering to Subsonic Aircraft Design in a University Environment |
C. BIL |
| DISAP - A Dialogue Orientated Process Planning System |
W. EVERSHEIM, J. AUGE, J. SCHULZ |
| Automated Structural Optimization at Warton |
R. I. KERR, D. THOMPSON |
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Testing of Composite Structures
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| Acoustic Emission and N.D.E. - Partners in Damage Detection During Strengtn Testing of Airframe Structures |
G. JACKSON, G.S. WHALLEY |
| Fibre Optic Damage Detection in Composite Structures |
B. ·HOFER |
| Fire Safety Investigations for Material Selection and Design of a Carbon Fibre Reinforced Fuselage Structure |
E. MIKUS |
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Performance
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| Wind Influence on the Range of Jet or Propeller Aircraft |
J.F. ELASKAR |
| Reducing Fuel Consumption by Cyclic Control |
G. SACHS, T. CHRISTODOULOU |
| Near-Optimal Feedback Control for Three-Dimensional Interceptions |
J. SHINAR, K.H. WELL, B. JÄRMARK |
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Shock / Boundary Layer Interaction
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| The Effects of Sweep and Bluntness on Glancing Interactions at Supersonic Speeds |
J.L. STOLLERY, N.R. FOMISON, S. HUSSAIN |
| Observations on the Turbulence Structure in an Unsteady Normal Shock/Boundary Layer Interaction |
L.C. SQUIRE, J.A. EDWARDS |
| Mean and Fluctuating Pressure Measurements in a Passive Controlled Shock/Boundary Layer Interaction |
S. RAGHUNATHAN |
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Unconvential Design
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| A Review of Unconventional Aircraft Design Concepts |
R.H. LANGE |
| The British Aerospace Experimental Aircraft Programme and the Role of System Development Cockpits |
P. V. WHITESIDE |
| The Impact of Emerging Technologies on an Advanced Supersonic Transport |
C. DRIVER, D.J. MAGLIERI |
| Lighter-Than-Air Aircraft as Control Configured Vehicle |
M. ONDA |
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Manufacturing
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| Airbus-Assembly Concepts to Improve Productivity and Flexibility in Aircraft Construction |
J. MASKOW |
| Fault Tolerant Systems |
I.W. NEWTON, T.G. HAMILL, R.A. GEORGE |
| Case Studies in Aircraft Manufacturing Automation |
G. L. MICHAELSON |
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Buckling and Postbuckling of Composites
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| The Design and Construction of a Post Buckled Carbon Fibre Wing Box Structure |
W.G. BROOKS |
| Compressive Buckling Strength of Graphite- Epoxy Laminated Curved Panels |
S. KOBAYASHI, K. SUMIHARA, K. KOY A MA |
| Analytical and Experimental Investigation on Advanced Composite Wing Box Structures in Bending Including Effects of Initial Imperfections and Crushing Pressure |
E. ANTONA, G. ROMEO |
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Active Control Technology
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| Active Flutter Suppression |
A. BRADSHAW, T. RAHULAN, M.A. WOODHEAD |
| Active Control Technology for Civil Transport |
H.P.Y. HITCH |
| Designing a Load Alleviation System for a Modern Civil Aircraft |
B.W. PAYNE |
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Computational Aerodynamics 1
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| High Order Solutions of the Euler Equations by Characteristic Flux Averaging |
A. EBERLE |
| Numerical Simulation of 3-D Inviscid Flow Fields around Complete Aircraft Configurations |
S. LEICHER, W. FRITZ |
| Efficient Solution of Three-Dimensional Euler Equations Using Embedded Grids |
R. RADESPIEL |
| Transonic Computations about Complex Configurations Using Coupled Inner and Outer Flow Equations |
U.G. NÄVERT, Y.C.-J. SEDIN |
| Application of the Tranair Full-Potential Code to Complete Configurations |
L.L. ERICKSON, M.D. MADSON, A.C. WOO |
| Optimum-Opti·morum Integrated Wing-Fuselage Configuration for Supersonic Transport Aircraft of Second Generation |
A. NASTASE |
| |
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High Angles of Attack 1 Multi-Element Airfoils
|
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| Calculation of Flow over Multielement Airfoils at High Lift |
T. CEBECI, K.C. CHANG, R.W. CLARK, N.D. HALSEY |
| The High Lift Development of the A320 Aircraft |
J. R. WEDDERSPOON |
| Potential Flow Models of Airfoils with Separated Flow |
G. V. PARKINSON, W. YEUNG |
| An Experimental Study of Turbulent Wake/Boundary Layer Mixing Flows |
L.J. JOHNSTON, H.P. HORTON |
| |
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Navigation
|
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| Global Integrated Communication, Navigation and Identification Based on Satellites |
G. PLÖGER, H. BERNER, G. HOFGEN |
| Low Cost Inertial Reference System Based on Fiber Gyros with GPS-Aiding |
D. RAHLFS |
| Test and Flight Evaluation of Precision Distance Measuring Equipment |
K. BECKER, A. MOLLER, K.H. HURRASS |
| Flight Management Concepts Compatible with Air Traffic Control |
S.A. MORELLO |
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|
Design with Composite Materials 1
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| Simplified Design of Composite Materials |
S.W. TSAI, J.M. PATTERSON |
| Materials in Aerospace - Can the Emerging Thermoplastics Meet the Challenge ? |
C. K. HALL |
| Properties and Potential of Multi-Directional- Fiber Composite Materials |
B. WALTER ROSEN |
| Advanced Polymer Composites for High Temperature Applications |
D. WILSON |
| |
|
Stability and Control / Handling Qualities 1
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| Precise Solution for Rational Transfer Parameters of Flight Vehicles |
Y. ZENG |
| Design Criteria for Flight Control Systems |
G. SCHÄNZER |
| Flight Simulation Techniques with Emphasis on the Generation of High Fidelity 6 DOF Motion Cues |
M. BAARSPUL |
| Handling Qualities for Unstable Combat Aircraft |
J.C. GIBSON |
| Validation of Nonstationary Aerodynamics Models for Longitudinal Aeroplane Motion on the Basis of Flight Measurements |
V. KOCKA |
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Computational Aerodynamics 2
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| Disordered Vortex Flow Computed around a Cranked Delta Wing at Subsonic Speed and High Incidence |
A. RIZZI, C.J. PURCELL |
| The Development of Practical Euler Methods for Aerodynamic Design |
R.H. DOE, T.W. BROWN, A. PAGANO |
| Algebraic Grid Generation about Wing-Fuselage Bodies |
R. E. SMITH |
| A Comparison of an Explicit and an Implicit Time Marching Method for Calculating Inviscid Internal Flows |
I. TEIPEL, A.R. WIEDERMANN |
| Application of a Full Potential Method to Practical Problems in Supersonic Aircraft Design and Analysis |
K. B. WALKLEY, G. E. SMITH |
| |
|
High Angle of Attack 2 / Vicious Flow
|
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| Boundary Layer Calculation and Viscous- Inviscid Coupling |
A.G. T. CROSS |
| Wake /Boundary Layer Interactions in Two and Three Dimensions |
L.C. SQUIRE, D. AGOROPOULOS, A.H.Kh. MOGHADAM |
| On the Duration of Low Speed Dynamic Stall |
R.A.McD. GALBRAITH, A.J. NIVEN, L.Y. SETO |
| |
|
Regulations
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| A Simulation Facility for Assessing the Next Generation of 4-D Air Traffic Control Procedures |
A. BENOIT, S. SWIERSTRA |
| Managing Airworthiness |
P. J. CRAWFORD |
| Certification of Advanced Experimental Aircraft |
W. BRADSHAW |
| |
|
Design with Composite Materials
|
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| Plastic or Metal - The Judgement Factors |
F.E. RHODES |
| Pressure Slip Casting of Ultrafine Powders - A Promising Processing for Ceramic-Ceramic Composites |
J.F. JAMET, M.H. RITTI |
| A Structural Modelling of Aeroelastic Composite Plates |
M.C. DÖKMECI |
| |
|
Stability and Control / Handling Qualities 2
|
|
| Experimental Study of Effects of Forebody Geometry on High Angle of Attack Static and Dynamic Stability and Control |
J.M. BRANDON, D.G. MURRI, L. T. NGUYEN |
| Aircraft Control with the Realization of Separate Motion Forms |
G. I. ZAGAYNOV, A. Z. TARASOV |
| Various Approaches in Solving Stability Problems for Symmetric Angle-Ply Laminates under Combined Loading |
M.J. JOSIFOVIC and V.Lj. RADOSAVLJEVIC |
| Flight Path Reconstruction - A Powerful Tool for Data Compatibility Check |
K.-O. PROSKAWETZ, R. BROCKHAUS |
| |
|
Computational Aerodynamics 3
|
|
| Leading Edge Vortex Flow over a 75 Degree-Swept Delta Wing - Experimental and Computational Results |
R. CARCAILLET, F. MANIE, D. PAGAN, J. L. SOLIGNAC |
| Free-Vortex Flow Simulation Using a Three- Dimensional Euler Aerodynamic Method |
P. RAJ, J.S. SIKORA, J.M. KEEN |
| Evaluation of Pressure Distributions on an Aircraft by Two Different Panel Methods and Comparison with Experimental Measurements |
A. BASTON, M. LUCCHESINI, L. MANFRIANI, L. POLITO, G. LOMBARDI |
| Finite-Volume and Integral-Equation Techniques for Transonic and Supersonic Vortex-Dominated Flows |
O.A. KANDIL, A. CHUANG, L. C. CHU |
| |
|
High Angles of Attack3 Vortex Flow
|
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| Effects of Spanwise Blowing on Pressure Distribution and Leading-Edge Vortex Stability |
J. ER-EL, A. SEGINER |
| Forebody Vortex Management for Yaw Control at High Angles of Attack |
D.M. RAO, C. MOSKOVITZ, D.G. MURRI |
| Prediction of the Aerodynamic Characteristics of Flight Vehicles in Large Unsteady Maneuvers |
M.R. MENDENHALL, S.C. PERKINS, D.J. LESIEUTRE |
| Analysis of Strake-Slender-Wing Configurations Using Slender-Wing Theory |
J. KRISPIN, H. PORTNOY |
| Analysis of the Vertical Flow around a 60 Degree Delta Wing with Vortex Flap |
B. SUNG, J.F. MARCHMAN |
| |
|
Maintenance
|
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| Avionics Fault Data Acquisition - A Concept for Civil Transport Aircraft |
T. STIER |
| Maintainability Optimization - The Future Challenge |
J. ROSE |
| |
|
Crash Testing
|
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| Structural Dynamics Research in a Full-Scale Transport Aircraft Crash Test |
H .G. McCOMB, R. G. THOMSON, R.J. HAYDUK |
| A Study of the Str,uctural Integrity of the Canadair Challenger at Ditching |
P.T. TO |
| Failure Analysis of Aircraft Windshields Subjected to Bird Impact |
A. SAMUELSON, L. SÖRNÄS |
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|
Model Testing
|
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| The Estimation of the Stability and Control Characteristics of a Canard Configured Combat Aircraft Having a Forward Swept Wing |
M.V. COOK, F. HEYDARI |
| Estimation of Aerodynamic Parameters from Flight Data of a High Incidence Research Model |
V. KLEIN, M.H. MAYO |
| Analysis of Externally-Piloted Vehicle Aircraft Model Flight Tests Using Aerodynamic Parameter Estimation Techniques |
E.R. WHITE |
| |
|
Wind Tunnel Methods 1 Wall Interference Effects
|
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| Advances at AEDC in Treating Transonic Wind Tunnel Wall Interference |
E.M. KRAFT, A. RITTER, M.L. LASTER |
| Numerical Design Parameter Study for Slotted Walls in Transonic Wind Tunnels |
N. AGRELL, B. PETTERSSON, Y. C.-J. SEDIN |
| Analysis of Wind Tunnel Corrections for Half-Model Tests of a Transport Aircraft Using a Doublet Panel Method |
M. MOKRY, J.R. DIGNEY, R.J.D. POOLE |
| Aeroacoustics at the German-Dutch Wind Tunnel |
H.H. HELLER, W.R. SPLETTSTOESSER, W.M. DOBRZYNSKI, K.-J. SCHULTZ |
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|
Fatigue and Damage Tolerance of Composites
|
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| Damage Tolerance of Composites |
J.E. McCARTY |
| Fatigue Crack Growth Predictions in Aramid Reinforced Aluminium Laminates (ARALL) |
R. MARISSEN |
| Spectrum Fatigue Model for Composite Laminates |
G.E. MABSON, N. PAPATHANASSIS, G.E. WHARRAM, R.C. TENNYSON |
| ExperimentaI and Numerical Analysis on Cracks Propagation in Aerospace Materials |
M. MARCHETTJ, F. MORGANTI, G. ANDRETTA, A. LA BARBERA |
| |
|
Airbreathing Engine Technology 1
|
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| Qualification of the Flow in Air Intakes and Evaluation of the Loss of Surge Margin Due to Distortions in the Compressor Inlet |
J. R. BION |
| Proposed Control of Compressor StalI by Pressure Perturbation and Blade Design |
B. S. THORNTON, L. C. BOTTEN, J.P. GOSTELOW |
| High Performance, Turbofan Afterburner Systems |
A. SOTHERAN |
| The Relationship between Turbofan Design and Geometry Parameters, Nacelle Configuration and its Drag |
S.P. ANDREEV, L.N. DRUZININ, M.M. TSHOVREBOV |
| |
|
Manufacturing and repair of Composites
|
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| Manufacturing Processes and Moulding of Fiber-Reinforced Polyetheretherketone (PEEK) |
G. KEMPE, H. KRAUSS |
| On the Fast Repair of Aircraft Panel Components |
S. DEHM, D. WURZEL |
| Automated Systems for the Manufacture of Airbus Vertical Stabilizer Spar Box in Composite Materials |
R. OBERFRANZ |
| Manufacturing Technology of Composite Torque Box of Vertical Fin |
Q. S. ZHAO et al |
| |
|
Windshear
|
|
| Safety Analysis of Automatic Landing through the Low Level Turbulent Wind |
S.X. ZHU, B. ETKIN |
| Take-Off and Landing in a Downburst |
K. -U. HAHN |
| Optimal Control Laws for Microburst Encounter |
R.F. STENGEL |
| Optimization and Gamma/Theta Guidance of Flight Trajectories in a Windshear |
A. MIELE, T. WANG, W.W. MELVIN |
| |
|
Wind Tunnel Methods 2 Flow Field Diagnostics
|
|
| Colour Helium Bubble Flow Visualization Technique |
D. ZHAO, Z. WANG, X. ZHANG, J. QIN, X. LANG |
| Measurements in Separating Boundary Layers |
M. DIANAT, I.P. CASTRO |
| Flow Field Study on a Supercritical Airfoil Using a Pressure Probe and a Two-Component Laser-Doppler-Anemometer |
K.A. BOTEFISCH, E. STANEWSKY |
| The F2 Wind Tunnel of the Fauga-Mauzac Test Center |
J.M. CHRISTOPHE |
| |
|
Metallic Materials
|
|
| Advances in Aluminium Alloys |
C.J. PEEL |
| A Review of the Development, Microstructure and Properties of New Al-Li Alloys |
E.A. STARKE, Jr |
| Single Crystal Superalloys for Turbine Blades in Advanced Aircraft Engines |
T. KHAN, P. CARON |
| Unified Constitutive Materials Model Development and Evaluation for High-Temperature Structural Analysis Applications |
R.L. THOMPSON, M.T. TONG |
| |
|
Airbreathing Engine Technology 2
|
|
| Computation of Unsteady Flows in Turbomachine Cascades |
A. FOURMAUX |
| Advances in Turbine Technology |
H. TUBBS, M.J. HOLLAND |
| The Role of Flow Field Computation in Improving Turbomachinery |
J. DUNHAM |
| |
|
Aerolasticity and Structural Dynamics 1
|
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| Aeroelastic Tailoring for Flutter Constraints |
J. SCHWEIGER, O. SENSBURG, C. PONZI |
| Active Damping of Airliner Pylon-Mounted Engine Elastic Vibrations |
A.F. MINAEV |
| On the Optimization of Flutter Characteristics of Laminated Anisotropic Cylindrical Shells |
G.V. VASILIEV |
| |
|
Safety
|
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| Experimental Investigation of Electrostatic Fire and Explosion Accidents after Aircraft Landing and Preventive Design |
H.S. LOU |
| The Airline Engineering Role in the Management of Safety |
D.K. CRAIG |
| Performance Evaluation of a Linear Recursive Technique for Aircraft Altitude Prediction in Airborn Collision Avoidance Systems |
A. BADACH, P. FORM |
| |
|
Boundary Layer Studies
|
|
| Disturbance Functions of the Gortler Instabil.ity on an Airfoil |
J.R. DAGENHART, S.M. MANGALAM |
| Numerical Requirements in the Calculation of Flow over Bodies of Revolution at Incidence |
T. CEBECI, A.A. KHATTAB, S.M. SCHIMKE |
| Drag Reduction Mechanisms Derived from Shark Skin |
D.W. BECHERT, M. BARTENWERFER, G. HOPPE, W.-E. REIF |
| |
|
Engine Control
|
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| The M53 Turbofan Control System: A Strong Basis for the Development of Future Digital Control Systems |
P. GALMICHE |
| Digital Engine Control Units for a Fighter Engine and an Auxiliary Power Unit A Comparison |
G. DAHL |
| Case Studies of the Effects on Non-Linearities on the Accuracy of Gas Turbine Control |
D.M. TURNER |
| |
|
Potential for Future Propfan Aircraft
|
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| A Propfan Status Report |
J. MORRIS |
| Propfan and Turbofan - Antagonism or Synthesis |
H. GRIEB, D. ECKARDT |
| Potential Application of Advanced Propulsion Systems to Civil Aircraft |
A. BLYTHE |
| |
|
Aerolasticity and Structural Dynamics 2
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| Integrated Structure/Control Design - Present Methodology and Future Opportunities |
T.A. WEISSHAAR, J.R. NEWSOM, T.A. ZEILER, M.G. GILBERT |
| A General Formulation for the Aeroelastic Divergence of Composite Sweptforward Wing Structures |
L. LIBRESCU, J. SIMOVICH |
| Research on Active Suppression Technology for Wing/Aileron Flutter |
D.M. ZHU, Z.Q. GU, M.H. CAN, Z.F. CHEN, W.P. WANG |
| Aeroelastic Tailoring of Aft-Swept High Aspect Ratio Composite Wings |
J.A. GREEN |
| Intersection of an Oblique Shock Wave with a Cylindrical Afterbody |
G.C. SHEN, D.R. PHILPOTT |
| |
|
Noise
|
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| Method for Determinating the ISO-Noise Levels by Simulated Aircraft Flight Operations |
A. SOBOR |
| Control of Interior Noise in Advanced Turbopropeller Aircraft |
A. CARBONE, A. PAONESSA, L. LECCE, F. MARULO |
| Active Noise Control |
C. F. ROSS |
| |
|
Wind Tunnel Methods 3 Flight Measurements
|
|
| The Prediction of Lift Inferred from Downstream Vorticity Measurements |
W. SEND |
| Effect of the Reynolds Number on a Transonic Flow around Profiles and Sections of a Swept Wing |
G.A. PAVLOVETS, V .M. GADETSKY |
| Method of Analysing Data on a Swept Wing Aircraft in Flight |
A. BERTELRUD, J. OLSSON |
| An Experimental Study of a Three Lifting Surface Configuration |
C. OSTOWARI, D. NAIK |
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|
Unsteady Aerodynamics
|
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| Applications of PotentiaI Theory Computations to Transonic Aeroelasticity |
J.W. EDWARDS |
| Steady and Unsteady Investigations of Spoiler and Flap Aerodynamics in Two Dimensional Subsonic Flows |
M. COSTES, A. GRAVELLE, J.J. PHILIPPE, S. VOGEL, H. TRIEBSTEIN |
| NASA's Aircraft Icing Analysis Program |
R.J. SHAW |
| Oscillating Wings and Bodies with Flexure in Supersonic Flow - Applications of Harmonic Potential Panel Method |
D.D. LIU, P. GARCIA-FOGEDA, P.C. CHEN |
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|
Propulsion / Airframe Integration
|
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| On the Computation of Wing Lift Interference Caused by High Bypass Engines |
C. HABERLAND, G. SAUER |
| Propulsion/Aerodynamic Integration in a STOVL Combat Aircraft |
G.M. APPLEYARD, J. COWPER |
| Utilization of Computation and Experiment for Airframe Propulsion Integration Development |
D.L. BOWERS, C.H. BERDAHL |
| Integrated Airframe/Propulsion Control System Architectures (IAPSA) Study |
C.M. CARLIN, A.D. STERN |
| Theoretical Considerations of the Specific Impulse of Ramjet Engines |
A. GANV |
| A Comparison of Pod and Tail Mounted Ramjets |
D.R.M. ARENS, H.V. HATTINGH |
| Regression Rate Study for a Solid Fuel Ramjet |
G. SCHULTE, R. PEIN |
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|
Fatigue and Dynamics of Structures 1
|
|
| The Control and Use of Residual Stresses in Aircraft Structural Parts |
B. JAENSSON, S.-E. LARSSON |
| A Comparison of Impulse and Random Tests from Modal Analysis of an Aeronautical Structure |
L. BALIS CREMA, A. CASTELLANI |
| Fatigue Fracture in Landing Gear Steels |
R.J.H. WANHILL |
| Fatigue Life Predictions under Complex Loading |
F.M. WU, B.F. ZHANG |
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|
Landing Gear
|
|
| New Design Procedures Applied to Landing Gear Development |
J. VEAUX |
| Shimmy Problems of Landing Gears Caused by Elastic Deformation of Tires |
E. SPERLING |
| Measurements of Landing Gear Loads of a Commuter Airliner |
A. I. GUSTAVSSON |
| Topics in Landing Gear Dynamics Research at NASA Langley |
H.G. McCOMB, J.A. TANNER |
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|
Applied Aerodynamics
|
|
| Take-Off Drag Prediction for the Airbus A-300-600 and the A310 Compared with Flight Test Results |
B. HAFTMANN, F.-J. DEBBELER, H. GIELEN |
| Wing Laminar Boundary Layer in the Presence of a Propeller Slipstream |
S.J. MILEY, R.M. HOWARD, B.J. HOLMES |
| Variable Wing Camber for Transport Aircraft |
u. GRAEBER |
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|
Hypersonics
|
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| Experimental and Theoretical Tests for Prediction of Aerodynamic Moments of HERMES in Hypersonic Flight |
P. VANCAMBERG |
| Rarefied Flow Lift-to-Drag Measurements of the Shuttle Orbiter |
R.C. BLANCHARD |
| Configuration and Trajectory of Hypersonic Transport with Aerothermodynamic Control |
Y. AIHARA, S. NOMURA, H. MINAKUCHI, A. MURAKAMI, N. SUDAN I |
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Turboprop Desogn Considerations
|
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| The Performance of Advanced Prop-Fan Transmission |
J. DOMINY |
| Prediction of Single-Rotation Prop-Fan Noise by a Frequency Domain Scheme |
H. GOUNET , S. LEWY |
| Calculations of High Speed Propeller Performances Using Finite Difference Methods |
M. KOBAYAKAWA, H. ONUMA, Y. SHIOTA |
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Fatigue and Dynamics of Structures 2
|
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| Some Aspects of the Reliability Analysis of Aircraft Structures |
D. ZHU, F. LIN |
| Load Examination of Vehicle-Body of Reinforced Cylindrical Shell in Case of Kinematic Load |
Z. SZABO, P. MICHELBERGER |
| Details of Analysis of Airplane Structure Acoustic Loading in Flight Testing |
E.V. ARNAUTOV |
| |
|
Subsystem Technology
|
|
| High Performance Adaptive Controller and Parameter Optimization for Flight Control Systems |
J, CHEN, Y. OU, Z. LU, J. LIAN, S. SU |
| The Development of a Fibre Optic Data Bus for Helicopters |
M.J. KENNETT |
| Recent In-Flight Data and Electromagnetic Response of an Aircraft Structure Struck by Lightning |
J.L. BOULAY |
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| In Memoriam |
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| The International Council of the Aeronautical Sciences |
|
| |
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| ICAS Program Committee |
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| ICAS Member Associations |
|
| ICAS Associate Members |
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