| Title |
Author(s) |
|
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| Space Transportation Systems |
G.B. MERRICK |
WRIGHT BROTHERS LECTURESHIP IN AERONAUTICS
|
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| How Decisions are Made: Major Considerations for Aircraft Programs |
J.E. STEINER |
ICAS-VON-KARMAN-LECTURE
|
|
| Engineering Aspects of International Collaboration on Tornado |
B.O. HEATH |
General lectures
|
|
| Tomorrow's Transport Aircraft A Part of a System. A System in its Own Right |
P. LECOMTE |
History Lecture
|
|
| A History of USA/Italy Mutual Exchange in the Field of Aeronautics |
M.F. CAPRONI-ARMANI |
| |
|
FIGHTER SYSTEMS OF THE FUTURE
|
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| Trends in Fighter Design A German View |
K. KNAUER |
| Advanced Aerodynamic Design for Future Combat Aircraft |
B.R.A. BURNS |
| Some Aerodynamic/Fl ightmechanic Aspects for the Design of Future Combat Aircraft |
P. MANGOLD |
| Increased Requirements for the Missile Aerodynamics Due to the Observer Technique |
G. GREGORIOU, H.-G. KNOCHE |
| |
|
Aerolasticity
|
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| Gust Load Alleviation on Airbus A 300 |
O. SENSBURG, J, BECKER, H. LUSEBRINK, F. WEISS |
| Calculations of Transonic Steady State Aeroelastic Effects for a Canard Airplane |
N. AGRELL, S.G. HEDMAN |
| Computer-Aided Derivation of Equations of Motion for Rotary-Wing Aeroelastic Problems |
F. KIESSLING |
| Hajif-11, A Program System for the Dynamic Analysis of Aeronautical Structures |
LIU GUO-GUANG, LI JUN-JIE |
| |
|
Crew Station Design
|
|
| Human Factor and Flight Safety |
J.C. WANNER |
| A Practical Approach to the Incorporation of Technical Advances in Avionics |
J. D. BANNISTER, D. ROUGHTON |
| Applying Advanced Technology to Flight Station Design |
W.R. PADEN, G.A. SEXTON |
| The Evolution of Display Formats for Advanced Fighters Using Multimode Colour CRT Displays |
N.M. LEFRITZ, J.H. TUTTLE, M.J. FORTE |
| |
|
Propulsion Systems 1
|
|
| Application of Advanced Exhaust Nozzles for Tactical Aircraft |
D.L. BOWERS, J.A. LAUGHREY |
| Optimized 10 Ton Class Commercial Aircraft Engine |
R. LAURENS |
| Recent Advances in the Performance of High Bypass Ratio Fans |
D.J. NICHOLAS, C. FREEMAN |
| Axisymmetric Approach and Landing Thrust Reverser Impacts on Usage and LCC |
J.P. BLACKMAN, P.B. STUMBO, M.F. EIGENMANN |
| |
|
Laminar Flow
|
|
| Observations and Implications of Natural Laminar Flow on Practical Airplane Surfaces |
B.J. HOLMES. C.J. OBARA |
| Aerodynamic Development of Laminar Flow Control on Swept Wings Using Distributed Suction Through Porous Surfaces |
J.A. THELANDER, J.B. ALLEN, H.R. WELGE |
| External Aerodynamic Design for a Laminar Flow Control Glove on a Lockheed Jetstar Wing |
J.A. BENNETT, L.B. BRANDT |
| NASA Research on Viscous Drag Reduction |
R.H. PETERSEN, D.V. MADDALON |
| |
|
Computational Aerodynamics 1
|
|
| Computational Fluid Dynamics Around Complete Aircraft Configurations |
P. PERRIER |
| Viscous Transonic Airfoil Flow Simulation |
J. LONGO, W. SCHMIDT, A. JAMESON |
| Computation of Supersonic Flow Around Three-Dimensional Wings |
B.G. ARLINGER |
| Transonic Small Disturbance Code for Body-Wing Configuration Coupled with Full Potential Code for Wing Alone |
A. LUNTZ |
| |
|
Developments in Fighter Technologies
|
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| Advanced Fighter Technology Integration Program AFTI/F-16 |
A.J. BIANCO, F.R. SWORTZEL |
| Tail Versus Canard Configuration - An Aerodynamic Comparison with Regard to the Suitability for Future Tactical Combat Aircraft |
G. WEDEKIND |
| Engine Implications for Supersonic Aircraft |
S.G. KYLE, G.G. UPTON, E. SCHREFFLER, M.B. SUSSMAN |
| |
|
Metal Structures and Power Plant Materials
|
|
| Material and Process Developments on the Boeing 767 |
J.T. QUINLIVAN, D.T. LOVELL |
The Promise of Laminated Metals in
Aircraft Design |
D.H. PETERSEN, L.E. SLOTER II,
W.A. POINDEXTER, J.L. MARIS, G.E. KUHN |
| Aluminium Bonding for Durable Structures |
J.D. ALLDREDGE, C.S. CARTER,
J.C. McMILLAN |
| |
|
Control Systems
|
|
| Design of Compensated Flutter Suppression
Systems |
M. LANZ, P. MANTEGAZZA |
| Design and Experience with a Low-Cost
Digital Fly-By-Wire System in the
SAAB JA37 VIGGEN A/C |
K. FOLKESSON. P.-O. ELGCRONA.
R. HAGLUN |
| Design and Flight Testing of a Digital Optimal
Control General Aviation Autopilot |
J,R, BROUSSARD. D.R. DOWNING.
W.H. BRYANT |
| Preliminary Design of an Advanced Integrated
Power and Avionics Information System |
G.L. DUNN,
P. LEONG,
D. FOX |
| |
|
Inlets and Nozzles
|
|
| Efficiency of a Top-Mounted Inlet System
at Transonic/Supersonic Speeds |
K. WIDING |
| Inlet and Airframe Compatibility for a V/STOL
Fighter/Attack Aircraft with Top-Mounted
Inlet |
D.A. DURSTON, D.B. SMELTZER |
| A Remote Augmentor Lift System with a
Turbine Bypass Engine |
L.H. FISHBACH, L.C. FRANCISCUS |
| |
|
Unsteady Aerodynamics
|
|
| Investigation of the Unsteady Airloads on a
Transport Aircraft Type Airfoil with Two
Interchangeable Oscillating Trailing Edge
Flaps. at Transonic Speed and High Reynolds
Numbers |
H. TRIEBSTEIN, R. DESTUYNDER,
H. HANSEN |
| Determination de l' Efficacite d ' un Vol et
de Bord de Fuite en Ecoulement Tridimensionnel
Instationnaire |
H. CONSIGNY |
| An Investigation of Scale Model Testing
of VTOL Aircraft in Hover |
W.G. HILL,Jr., R.C. JENKINS,
M. R. DUDLEY |
| Optimisation du Vol a Aile Battante |
P. CONTENSOU |
| |
|
Computational Aerodynamics 2
|
|
| Recent Developments in Computation of
Strongly Interacting Flows |
L.G. NAPOLITANO, R. MONTI |
| Computation of Low Speed Fl ow Past
Multi-Element Airfoils with Large
Flow Separation |
G.W. ZUMWALT, R. ELANGOVAN |
| Calculation of Vortex Flows on Complex Configurations |
B. MASKEW. B.M. RAO |
| |
|
Unique Commuter Aircraft Designs
|
|
| Design Criteria for Utility/Commuter Aircraft |
J. SPINTZYK, H. KROJER, H. LIESE |
| Ultra STOL Derivative Design of a Sea-Based CTOL Aircraft |
Y. T. CHIN |
| Advanced Technologies Applied to Reduce the Operating Costs of Small Commuter Transport Aircraft |
O. MASEFIELD, A. TURI, M. REINICKE |
| |
|
Damage Tolerance And Fatigue
|
|
| The Damage Tolerance Approach to the Canadair CL-600 Challenger |
D.R. TURNER, C. MANDERS |
| High Cycle Fatigue of Metal Structures The Fatigue Threshold Concept |
A. F. BLOM. J. BÖCKLUND |
| Design and Experimental Verification of the USB-FLAP Structure for NAL STOL Aircraft |
M. SANO, Y. FUJIMORI, S. MAEKAWA |
| |
|
Space Shuttle
|
|
| Effects of System Interactions on Space Shuttle Loads and Dynamics |
R.E. GATTO |
| Correlation of Flight and Wind Tunnel Stability and Control Aerodynamics of the Space Shuttle Orbiter |
J.M. UNDERWOOD |
| The Shuttle Mission Simulator Visual Imagery |
T. H. HENDERSON |
| |
|
Analytical Techniques for Propulsion Systems
|
|
| Computational Methods for Two-Dimensional and Three-Dimensional Inlets in Subsonic and Supersonic Flow |
J. GRASHOF, W. SCHMIDT |
| A Summary of V/STOL Inlet Analysis Methods |
D.P. HWANG, J.M. ABBOTT |
| Ejector Nozzle Development |
E.F. SCHUM. J.H. DeHART, P.M. BEVILAQUA |
| |
|
Experimental Methods in Aerodynamics
|
|
| The Application of Photon Correlation Laser Velocimetry to Turbulent Flow Field Investigations |
G.D. CATALANO, H.E. WRIGHT |
| Research for the Visualization of Transitional and Other Turbulent Phenomena in a Boundary Layer |
S.X. LI, Y. SHEN, Y.D. SHI |
| A Unique Flight Test Facility: Description and Results |
R.R. MEYER, Jr |
| |
|
Computational Aerodynamics 3
|
|
| Finite Difference Computation of Airfoils with Blunt Noses in Transonic Flows |
D.Q. WANG |
| Some Theoretical Wal-Interference Calculations in Slotted Transonic Test-Sections, Three- Dimensional Flows |
Y. C-J. SEDIN, K.R. KARLSSON |
| Determination of Airplane Aerodynamic Parameters from Flight Data at High Angles of Attack |
V. KLEIN, J.G. BATTERSON |
| A Direct Approach for the Panel Method in Compressible Flows |
A. DAS |
| Computational and Experimental Studies of Light Twin Aerodynamic Interference |
W.G. THOMSON, W.H. WENTZ, C. OSTOWARI |
| |
|
Advanced Technologies for General Aviation
|
|
| The Design Genesis and Development of the Peregrine II |
R.J. STEWART |
| Dual Wing, Swept Forward Swept Rearward Wing, and Single Wing Design Optimization for High Performance Business Airplanes |
M.D. RHODES, B.P. SELBERG |
| Assessment of Advanced Technologies for High Performance Single-Engine Business Airplanes |
O.L. KOHLMAN, B.J. HOLMES |
| The Design Integration of Wingtip Devices for Light General Aviation Aircraft |
R.V. GIFFORD, C.P. VAN DAM |
| Summary of Research Concerning Single Pi lot IFR Operational Problems |
S. WEISLOGEL |
| |
|
Composite Structures 1
|
|
| Operation VlOF - Development of a Composite Material Wing |
G. HELLARD, D. CHAUMETTE |
| A One-Shot Autoclave Manufacturing Process for Carbon Epoxy Components |
M. KAITATZIDIS, R. RENZ, D. WURZEL |
| Non-Honeycomb F-16 Horizontal Stabilizer Structural Design |
D.N. BUTCHER |
| Material Identification for the Design of Composite Rotary Wings |
V. GIAVOTTO, C. CAPRILE, M. DE CAPITANI, L. SALVIONI, V. CARAMASCHI, G.C. MAFFIOLI, F. MUSSI |
| Studies on Optimization of Laminated Composite Plates |
S.P. JOSHI, N.G.R. IYENGAR |
| |
|
Flight Management And Landing Aids
|
|
| Dynamic Energy Transfer Between Wind and Aircraft |
G. SCHANZER |
| Digital Computer Simulation of Modern Aeronautical Digital Communication Systems |
CHOW SUMCHEONG |
| Flight Simulation Studies on the Feasibility of Laterally Segmented Approaches in an MLS Environment |
L.J.J. ERKELENS |
| A Concept for 4D-Guidance of Transport Aircraft in the TMA |
V. ADAM, W. LECHNER |
| Optimal Open-Loop Aircraft Control for Go-Around Maneuvers under Wind Shear Influence |
H.G. JACOB |
| |
|
Rotorcraft / Component Design
|
|
| The Nonsynchronous Whirls of the Turbine Rotor in Aerojet Engines |
GU JIA-LIU, REN PIN-ZHEN |
| Fluctuating Forces and Rotor Noise Due to Distorted Inflow |
G. NEUWERTH, R. STAUFENBIEL, A. KELLNER, J. SCHREIER |
| An Experimental and Numerical Study of 3-D Rotor Wakes in Hovering Flight |
M. NSIMBA, D. FAVIER, C. MARESCA |
| Aerodynamic Interactions Between a 1/6-Scale Helicopter Rotor and a Body of Revolution |
M.D. BETZINA, P. SHINODA |
| The Prediction of Propeller/Wing Interaction Effects |
A.S. ALJABRI |
| |
|
Windtunnel Techniques
|
|
| Wind-Tunnel Testing of V/STOL Configurations at High Lift |
W R. SEARS |
| Modeling, Control, and Optimization Studies of the Langley 0.3-Meter Transonic Cryogenic Wind Tunnel |
J.J. THIBODEAUX |
| Estimation of Simulation Errors in the European Transonic Wind Tunnel (ETW) |
B. WAGNER |
| Experimental Works in the NAL High Reynolds Number Two-Dimensional Transonic Wind Tunnel on Advanced Technology and NACA Airfoils |
K. TAKASHIMA |
| Transonic Tests in a Wind Tunnel with Adapted Walls |
U. GANZER, Y. IGETA |
| Prediction of High Alpha Flight Characteristics Utilizing Rotary Balance Data |
W. BIHRLE. Jr |
| |
|
Aerodynamic Drag
|
|
| On the Application of a Two-Equation Turbulence Model to the Solution of the "Time-Averaged" Navier-Stokes Equations |
R.U. JETTMAR, J.C. ROTTA |
| Wall Shear Stress Determination in Boundary Layers with Unknown Law of the Wall by a Modified Preston Tube Method |
C. HABERLAND. W. NITSCHE |
| Experimental and Theoretical Studies of Three-Dimensional Turbulent Boundary Layers on an Empennage of a Typical Transport Airplane |
H.C. SEETHARAM, N.J. PFEIFFER, M. OHMURA, J.D. McLEAN |
| Drag Determination and Analysis from Three- Dimensional Wake Measurements |
J.E. HACKETT, J.C. WU |
| On the Prediction of Induced Drag of Slender Wings with Flaps up to Transonic Mach Numbers |
W. KRAUS |
| |
|
Fuel Efficient Transports
|
|
| Requirements and Trends in Fuel Consumption in Transport Mission with Aircraft and Surface Vehicles |
G. GABRIELLI |
| Aerodynamic Concepts for Fuel-Efficient Transport Aircraft |
G. KRENZ, R. HILBIG |
| Progress at Douglas on Laminar Flow Control Applied to Commercial Transport Aircraft |
W.E. PEARCE |
| |
|
Fracture Mechanics
|
|
| Cracks Interacting with Contact Forces - A Finite Element Study on Loaded Holes |
H. ANSELL. B. FREDRIKSSON |
| Singular Propagation Behaviour of Cracks in Stiffened Cylindrical Shells |
CHANG SHANG CHOW |
| A New Testing Method of Impulsive Behaviour for Aerospace Materials |
K. KAWATA. S. HASHIMOTO, N. TAKEDA |
| A Crack Growth Model under Spectrum Loading |
YANG BING-XIAN |
| |
|
Maintenance
|
|
| Age Exploration in Naval Aviation |
A.D. WILLIAMS |
| Logistics Research Program in the United States Air Force |
J.C. REYNOLDS, P.E. DAVIDSON |
| F/A-18 R&M Does Early Planning Pay Off? |
R.D. DIGHTON |
| |
|
Propulsion Systems 2
|
|
| Third Generation Turbo Fans |
J.F. COPLIN |
| Turboprop Design - Now and the Future |
B.S. GATZEN |
| A Comparative Engine/ Airframe Integration Study of Advanced Technology General Aviation Powerplants |
D.R. ELLIS, G.L. HUGGINS, A. A. MUELLER, J. D. HEMBREY |
| |
|
Low Reynolds Number Aerodynamics
|
|
| Inflated Wings |
A. ROSELLI |
| Design and Tests of Airfoils for Sailplanes with an Application to the ASW-198 |
L.M.M. BOERMANS, H.J.W. SELEN |
| Variable Geometry Aerofoi 1 s as Applied to the Beatty 8-5 and 8-6 Sailplanes |
R. A. STREATHER |
| |
|
High Lift Aerodynamics
|
|
| Development of the Circulation Control Wing / Upper Surface Blowing Powered-Lift System for STOL Aircraft |
M.J. HARRIS, J.H. NICHOLS, Jr •• R.J. ENGLAR. G.G. HUSON |
| Ejector Powered Propulsion and High-Lift Subsonic Wing |
R.A. SQUYERS, J.L. PORTER, K.S. NAGARAJA, G.F. CUDAHY |
| Theoretical and Experimental Studies of Leading Edge Devices at Transonic Speeds |
G. VOLPE |
| Development of an Advanced No-Moving-Parts High-Lift Airfoil |
R. J. ENGLAR |
| |
|
Directions in Sea Based Aircraft
|
|
| Design Integration of CCW/USB for a Sea-Based Aircraft |
H.S.D. YANG, J.H. NICHOLS Jr |
| An Integrated Aerodynamic/Propulsive Design for a STOVL Fighter Attack/Aircraft |
W. H. FOLEY |
| Aircraft Design for Fuel Efficiency |
L.O. LEHMAN, D. WOLL, C. LAMPART |
| Performance Characteristics of a Buoyant Quad-Rotor Research Aircraft |
B.L. NAGABHUSHAN. P.P. JACOBS, C.E. BELKNAP, D.A. EULER |
| |
|
Composite Structures 2
|
|
| Application of a New Hybrid Material (ARALL) in Aircraft Structures |
J.W. GUNNINK. L.B. VOGELESANG, J. SCHIJVE |
| The Behaviour of Composite Thin-Walled Structures in Dynamic Buckling Under Impact |
J, ARI-GUR. J. SINGER, H. RÖHRLE |
| Nondestructive Testing in Aircraft Construction Using Holographic Methods |
K. WANDERS, H. STEINBICHLER |
| Design and Fabrication of Cocured Composite Hat-Stiffened Panels |
G.D. PEDDIE, E.E. SPIER |
| |
|
Flight Mechanics
|
|
| Spin Behaviour of the Pilatus PC-7 Turbo Trainer |
P. WITTWER. 0. MASEFIELD |
| Classification in Flight Mechanics |
V. KOCKA |
| Dynamics of Flexible Aircrafts: Numerical Examples on Simplified Model |
L. BALIS CREMA. A. CASTELLANI |
| Three Dimensional Mathematical Model of the Control System of a Homing Missile and Missile-Target Intersection Equations |
DONG BING-YING |
| |
|
Subsystem Technology 1
|
|
| Models for the Motor State of VSCF Aircraft Electrical Power System |
QIU XIANCHENG, YAN YANGUANG, HU YUWEN |
| The Effect of Intake Flow Disturbances on APU Compressor Blade High Cycle Fatigue in the Airbus A 300 |
K.W. LOTTER, J. J'ORG |
| Engine Controls for the 1980s and 1990s |
V. A. FISHER |
| |
|
Aerodynamic Design 1
|
|
| Advanced Aerodynamic Wing Design for Commercial Transports - Review of a Technology Program in the Netherlands |
N. VOOGT, J.W. SLOOFF |
| Recent Airfoil Developments at DFVLR |
H. KORNER, G. REDEKER |
| Wing-Tip Jets Aerodynamic Performance |
J.M. WU, A. VAKIL, Z.L. CHEN |
| |
|
Vortex Flows 1
|
|
| Vortex Flow Correlation |
G.E. ERICKSON |
| An Experimental Investigation of Leading-Edge Spanwise Blowing |
SU WENHAN, LIU MOUJI, ZHOU BOCHENG, QIU CHENGHAO, XIONG SHANWEN |
| Vortex Formation over Double-Delta Wings |
U. BRENNENSTUHL, D. HUMMEL |
| |
|
Making CAD/CAM Pay-Off
|
|
| CATIA: A Computer Aided Design and Manufacturing Tridimensional System |
F. BERNARD |
| CDS - The Designer's Media, The Analyst's Model |
D.P. RAYMER, S.K. ALBRECHT |
| Aircraft Geometry Verification with Enhanced Computer Generated Displays |
J.V. COZZOLONGO |
| |
|
Composite Structures 3
|
|
| Composite Materials Influences on Aeroelastic and Structural Design |
R. BARBONI, I. PERONI, N. BANITCHUK |
| Technical and Economic Comparison of Carbon Fiber Tape and Woven Fabric Applications |
G. HILAIRE, G. BRIENS |
| Application of Composite Materials and New Design Concepts for Future Transport Aircraft |
R.H. LANGE, J.W. MOORE |
| |
|
Rotor and Blade Design
|
|
| Shock-Free Airfoil, Wing and Turbojet Blade Design |
A.R. SEEBASS, K.-Y. FUNG, H. SOBIECZKY |
| Sliced Disc Design - A Composite Conform Concept for a Turbo Engine Axial Compressor? |
R. KOCHENDURFER |
| Comparison of HP Turbine "Deep Blade Design" Effects in Turbofan Engine Gas Generators with Different Bearing Structure Configurations |
D. RIST |
| |
|
Subsystem Technology 2
|
|
| An Alternative Approach to Engine Rating Structures Using Monitoring Systems |
D. LEWIS |
| Infrared Scanning for Improved Maintenance of Electronics Systems |
G.S. EGAN |
| Redundant Control Unit for an Advanced Multispool Engine |
G. DAHL |
| |
|
Aerodynamic Design 2
|
|
| Test Results of Chordwise and Spanwise Blowing for Low-Speed Lift Augmentation |
G.A. HOWELL |
| Aerodynamic Research Applications at Boeing |
A.L. NAGEL |
| Wind Tunnel Test and Aerodynamic Analysis of Three Aeroelastically Tailored Wings |
W.W. BRAYMEN, W.A. ROGERS, M.H. SHIRK |
| |
|
Vortex Flows 2
|
|
| Upper Vortex Flap - A Versatile Surface for Highly Swept Wings |
D.M. RAO |
| Analytical Study of Vortex Flaps on Highly Swept Delta Wings |
N.T. FRINK |
| Wind-Tunnel Investigation of Vortex Flaps on a Highly Swept Interceptor Configuration |
W.E. SCHOONOVER, Jr., W.E. OHLSON |
| Spanwise Distribution of Vortex Drag and Leading-Edge Suction in Subsonic Flow |
S. N. WAGNER |
| Fuselage Effects in Leading Edge Vortex Flap Aerodynamics |
J.F. MARCHMAN, M.L. HOLLINS |
| |
|
Future transport technology
|
|
| New Technology for the Next Generation of Commercial Transports - Real or Imaginary? |
I.S. MACDONALD |
| Advanced Turboprop Transport Development - A Perspective |
M.A. BOOTH, G.E. LEDBETTER, L.B. GRATZER |
| An Initial Look at the Supersonic Aerodynamics of Twin-Fuselage Aircraft Concepts |
R.M. WOOD, S.M. DOLLYHIGH,D.S. MILLER |
| |
|
Structural Dynamics
|
|
| Reduced Nonlinear Flight Dynamic Model of Elastic Structure Aircraft |
J. JANKOVIC |
| Determination of Load Spectra and Their Application for Keeping the Operational Life Proof of Sporting Airplanes |
H.J. KOSSIRA |
| The Role of the Scale Parameter in Service Load Assessment and Simulation |
J. GEDEON |
| Prediction of Critical Speeds of Flexible Support-Rotor Systems by Subsystem Impedance Analysis |
HUANG TAI-PING |
| Theoretical and Experimental Investigation of Joint-Structural Damping Interaction for Airplane Construction |
I.N. KRIVOSIC |
| |
|
Manufacturing and Maintenance
|
|
| Optimizing Aerospace Structures for Manufacturing Cost |
B.R. NOTON |
| Composite Structures Repair |
H. WICKER |
| Principles of Achieving Damage Tolerance with Flexible Maintenance Programs for New and Aging Aircraft |
J. HALL, U.G. GORANSON |
| Materials and Process Development Efforts in Support of the Air Force Maintenance Program |
J.A. SNIDE, B. DOBBS |
| |
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Inlet Vortices and Propulsion Simulation
|
|
| Intake Swirl - A Major Disturbance Parameter in Engine/Intake Compatibility |
F. AULEHLA |
| An Experimental Study of Strength and Existence Domain of Ground-to-Air Inlet Vortices by Ground Board Static Pressure Measurements |
S. O. RIDDER, I. SAMUELSSON |
| An Improved Propulsion System Simulation Technique for Scaled Wind Tunnel Model Testing of Advanced Fighters |
M.F. EIGENMANN, P.A. DEVEREAUX, C. D. WAGENKNECHT |
| |
|
Aerodynamic Design 3
|
|
| Low-Speed Characteristics of a Fighter-Type Configuration at High Angles-of-Attack and Sideslip |
K. HUENECKE |
| Wing Design for Supersonic Cruise/Transonic Maneuver Aircraft |
P. B. GINGRICH, E. BONNER |
| STOL Wind Tunnel Test Results for a Tactical Supercruiser |
R.A. HUTCHISON, M.B. SUSSMAN, R. MAINQUIST, J .W. PAULSON |
| Analysis of Jet Transport Wings with Deflected Control Surfaces by Using a Combination of 2- and 3-0 Methods |
N.J. PFEIFFER |
| |
|
Canard Configurations
|
|
| Optimization of Canard Configurations -An Integrated Approach and Practical Drag Estimation Method |
I.M. KROO, T. McGEER |
| Wind-Tunnel Investigation of a Full-Scale Canard-Configured General Aviation Aircraft |
L.P. YIP, P.F. COY |
| Wind Tunnel Measurements of Longitudinal Stability and Control Characteristics of Primary and Secondary Wing Configurations |
H.L. CHEVALIER |
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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 |
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