Feasibility of Gravity Gradient Technology for Fighter Aircraft (English)
- New search for: Blaylock, J. G.
- New search for: Swihart, D. E.
- New search for: Barfield, A. F.
- New search for: American Institute of Aeronautics and Astronautics
- New search for: International Council of Aeronautical Sciences
- New search for: Blaylock, J. G.
- New search for: Swihart, D. E.
- New search for: Barfield, A. F.
- New search for: American Institute of Aeronautics and Astronautics
- New search for: International Council of Aeronautical Sciences
In:
International Council of Aeronautical Sciences
;
562-568
;
1996
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ISBN:
- Conference paper / Print
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Title:Feasibility of Gravity Gradient Technology for Fighter Aircraft
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Contributors:Blaylock, J. G. ( author ) / Swihart, D. E. ( author ) / Barfield, A. F. ( author ) / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences
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Conference:Congress; 20th, International Council of Aeronautical Sciences ; 1996 ; Sorrento; Italy
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Published in:ICAS PROCEEDINGS ; 20//v1 ; 562-568
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Publisher:
- New search for: ICAS
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Publication date:1996-01-01
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Size:7 pages
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Remarks:Vol 1 of an unknown no of vols
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ISBN:
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Type of media:Conference paper
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Type of material:Print
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Language:English
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Keywords:
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Source:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Table of contents conference proceedings
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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A Cartesian Cut Cell Method for Unsteady Flows Involving Freely Moving BodiesYang, G. / Causon, D. M. / Ingram, D. M. / Saunders, R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 12
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Numerical Investigation of Strongly Non-Linear Transonic Flow Problems around the AirfoilYamamoto, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 19
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Solution of the Navier-Stokes Equations for the Flow around an Aerofoil in an Oscillating Free StreamShaw, S. / Qin, N. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 30
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Special Issues in Unsteady Navier-Stokes Simulations with Deforming BodiesHoffren, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 41
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Challenges and Opportunities in Fluid Mechanics ResearchHefner, J. N. / Sellers, W. L. / Thomas, J. L. / Wlezien, R. W. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 55
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Study for Reynolds Number Effect on C~i~m~a~x of 2-Dimensional AirfoilsYoshida, K. / Ogoshi, H. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 66
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Experimental Study on Transonic Shock Wave/Turbulent Boundary Layer Interactions and Separation Instabilities. Suction and Reynolds Number EffectsCaruana, D. / Bulgubure, C. / Mignosi, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 76
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A Review of Research at DRA on Active and Passive Control of Shock WavesAshill, P. R. / Fulker, J. L. / Simmons, M. J. / Gaudet, I. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 88
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On Sound Transmission through Boundary Layers of Aircraft Fuselages and Engine DuctsCampos, L. M. B. C. / Oliveira, J. M. G. S. / Serrao, P. G. T. A. / Kobayashi, M. H. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 99
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The Study of Wing-Rock Characteristics on Slender Delta Wings at High AOAHsiao, F.-B. / Yang, J.-S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 108
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Flow Analysis and Control Surface Evaluation at High Angels Attack for Enhanced ManoeuvrabilityTristrant, D. / Renier, O. / Farcy, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 118
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Flight Dynamics of a Vectored Thrust AircraftGranasy, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 122
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Determinants of Emission from Ground Operations of AircraftCaves, R. E. / Jenkinson, L. R. / Brooke, A. S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 131
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Methods to Asess Aircraft Engine Emissions in FlightDeidewig, F. / Doepelheuer, A. / Lecht, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 142
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Soot Emissions from Jet AircraftLilenfeld, H. V. / Whitefield, P. D. / Hagen, D. E. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 147
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NASA Noise Reduction Programs for Advanced Transport AircraftStephens, D. G. / Powell, C. A. / Cazier, F. W. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 155
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Civil Aircraft and Their Noise Impact on the Environment of the Athens-Spata AirportYiparakis, N. J. / Lambrianidis, G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 160
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Optimisation of Highly Loaded JointsRispler, A. R. / Steven, G. P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 167
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Structure Design Concepts for the Next Generation Supersonic TransportErmanni, P. / Braidley, I. / Ribere, B. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 175
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Bird Impact Resistance of Small Transport AircraftBedrich, L. / Mertl, V. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 183
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Development of a Structural RPV Section Serving as an Integral Fuel Tank made of Sandwich CFRPGali, S. / Ghilhai, G. / Peled, D. / David, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 191
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A Generic Architecture for In-Flight Crew Assistant Systems Based on Advanced Information Processing TechnologyZuidgeest, R. G. / Urlings, P. J. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 202
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A New Design Approach for a Pilot Advisory System in Air-to-Air InterceptionsYaakov, Y. / Shinar, J. / Wolfshtein, M. / Boneh, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 210
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An Al Situational Pilot Model for Real-Time ApplicationsBurdun, I. Y. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 238
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The Cost Effective Head-Up Display in Trainer AircraftSpring, H. / Inaebnit, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 243
-
Modelling and Identification of Non-Linear Unsteady Aerodynamic Loads by Neural Networks and Genetic AlgorithmsMarques, F. / Anderson, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 252
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Simulation of Unsteady Aerodynamic Effects of Isolated Vortices Close to the AirfoilMitrovic, C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 262
-
Numerical Simulations of Large Eddies in the Compressible Mixing-LayerRamella, F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 271
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Wall Turbulence Manipulation by Outer Layer DevicesReisoli-Matthieu, F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 278
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Helicopter Rotor Downwash Calculation using the Vortex Element Method for the Wake ModellingPapanikas, D. G. / Spyropoulos, A. J. / Fertis, D. K. / Margaris, D. P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 290
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Application of an Unsteady Two-Equation Turbulence Model to the Numerical Prediction of the Transonic Buffet of an AirfoilArina, R. / Ceresola, N. / Pianta, P. G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 297
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Cyclic Acceleration Technique for Solving Unsteady Transonic Small Perturbation EquationsWayan Tjatra, I. / Wandana, I. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 303
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NonEquilibrium ReentryFilatyev, A. S. / Yanova, O. V. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 314
-
Chattering Arc in Three-Dimensional FlightChern, J.-S. / Chen, Y.-H. / Hong, Z.-C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 325
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Aerodynamic Stabilization System for Small SatellitesSarychev, V. A. / Camelier, I. A. / Paglione, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 330
-
Theoretical and Experimental Determination of Flight Performances of an Airplane in Martian Atmospheric FlightTeofilatto, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 336
-
Flight Safety Aspects with Modern Flight Control SystemsChatrenet, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 341
-
Fly-By-Wire for the Saab 2000 - Concept, Development and TestingSinger, G. / Persson, U. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 351
-
Application of the Fuzzy Logic Control Theory to the Design of Aircraft Flight Control SystemsZhou, Z. Q. / Reichert, G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 359
-
Method for Determining the Force Characteristics of a Nozzle under the Exposure to External Supersonic FlowLokotko, A. V. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 368
-
High Altitude Long Endurance (HALE) UAV for Intelligence MissionsTsach, S. / Yaniv, A. / Avni, H. / Penn, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 380
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Development Approach of the HERON Medium Altitude Long Endurance UAVVitali, J. / Tsach, S. / Avni, H. / Gali, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 391
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Designing Process of Unmanned Aerial VehiclesJaxa-Malachowski, R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 398
-
The Use of Genetic Algorithms in Dynamic Finite-Element Model Identification for Aerospace StructuresDunn, S. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 407
-
Nonlinear Finite Element Analysis of Fluttering Plate in Transonic Unsteady Potential FlowsWayan Tjatra, I. / Kurniawan, R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 414
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Use of Artificial Neural Network for the Evaluation of SEA Coupling Loss Factor and AHL Damping ParametersSorrentino, A. / Vitiello, P. / Romano, G. / Dovstam, K. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 423
-
Rear Fuselage Flow Characteristics for a Complete Wing-Body Configuration at Transonic ConditionsCoustols, E. / Seraudie, A. / Mignosi, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 434
-
Theoretical and Experimental Studies of Vectoring Jets Effects on Under-Wing Stores and their Release TrajectoriesNangia, R. K. / Ross, J. A. / Peto, J. W. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 446
-
Aerodynamic Assessment of Lateral Jet Sheets and Their Influence on Wing-Body Combinations for some Blowing ArrangementsNeamtu, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 457
-
Canard Influence on the Boundary Layer of a Forward Swept WingLombardi, G. / Morelli, M. / Waller, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 466
-
Mean Characteristics of Flow in Junctures of Swept Wings and BodiesKhan, M. J. / Ahmed, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 472
-
A Linear Stability Analyser Suitable for Integration in Wing Performance Calculation ProceduresMasson, C. / Langlois, M. / Parashivoiu, I. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 483
-
Numerical Investigation of the Effects of Sweep Angle on the Boundary-Layer Transition in High Speed FlightShahpar, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 494
-
Transition Control on a Transonic Laminar Airfoil with Suction PanelJoergensen, L. / Nitsche, W. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 504
-
Hybrid Laminar Flow Nacelle DesignLecordix, J. L. / Mullender, A. / Lecossais, E. / Godard, J. L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 521
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A New Reconfiguration Concept for Flight Control Systems in Case of Actuator and Control Surface FailuresBaumgarten, C. / Heine, W. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 532
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On Some Analytical Studies of Unsteady and Non-Linear Longitudinal StabilityCampos, L. M. B. C. / Azinheira, J. R. C. / Fonseca, A. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 541
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Integrated T & E Approach to Store Separation - Dim Past, Exciting FutureCenko, A. / Richardson, P. / Talbot, M. / Loezos, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 552
-
Gust Alleviation Analysis for Flexible Wing-Tail ConfigurationsGennaretti, M. / De Troia, R. / Tancredi, G. / Morino, L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 562
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Feasibility of Gravity Gradient Technology for Fighter AircraftBlaylock, J. G. / Swihart, D. E. / Barfield, A. F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 569
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On the Development of Flexible Aircraft Equations of MotionRo, K. S. / Barlow, J. B. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 585
-
Dihedral Effect for Straight Tapered and Twisted WingsGili, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 593
-
Optimal Midcourse Trajectories for Precision Guided Munitions with Collocation and Nonlinear ProgrammingTekinalp, O. / Arslan, E. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 601
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Conceptual Design and Proposed Development of the GAP-4 Multi-Purpose Small Utility HelicopterSchrage, D. P. / Yillikci, Y. K. / Phillips, J. W. / Mavris, D. N. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 611
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Hover Performance of a Rotor with Deployable FlapsNagabhushan, B. L. / Shaban, A. I. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 619
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The Development of a Knowledge Based System to Aid Helicopter Rotor Blade DesignHamilton, J. R. / Clarkson, P. J. / Burgess, S. C. / Newland, D. E. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 631
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Wind Tunnel Testing of a 1/3rd Scale Model GyroplaneCoton, F. N. / Smrcek, L. / Patek, Z. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 640
-
Feasibility Study and Mission Requirement for HSCTMizuno, H. / Hagiwara, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 643
-
Special-Purpose Programs for Structural Design and OptimizationRothwell, A. / Heerschap, M. E. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 654
-
Analysis of Measured In-Flight Tail LoadsVan Gelder, P. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 665
-
Theoretical Assessment, Numerical Simulation and Comparison with Tests of Birdstrike on Deformable StructuresAnghileri, M. / Sala, G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 675
-
Strength Estimation Method for Undamaged, Damaged and Repaired Honeycomb StructuresUrinovsky, V. / Coldbeck, D. P. / Smrcek, L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 682
-
Heavy Transport Aircraft Reliability StudyChiesa, S. / Gianotti, P. / Maggiore, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 691
-
GMADS - Groundbased Maintenance Aid and Diagnostic SystemStenmarck, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 695
-
Turbojet Engine Diagnostic System based on Compressor Blade Vibration and Vibroacoustic AnalysisDabrowski, H. / Kudelski, R. / Spychala, J. / Szczepanik, R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 702
-
Extension in Calendar Life Limit for Aircraft StructureAhmad, M. / Ghafoor, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 710
-
Application of an Improved Integral Turbulent Boundary Layer Model with Moderate Separation Correction on NACA Series and Low Speed Supercritical Airfoil DerivativesKostic, I. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 719
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An Inverse Method for the Design of AirfoilsNagaoka, T. / Morishita, E. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 725
-
Theoretical Study of a Mission Adaptive WingMartins, A. L. / Catalano, F. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 733
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Using the Fluent Program for Optimisation of the Fowler Flap System for the Ultra-Light AeroplaneStrnad, B. R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 743
-
Progress in the Development of Computational Aerodynamic Design Methods: Inverse ProceduresMalone, J. B. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 753
-
Turbulent Flow Calculations for Complex Aircraft Geometries using Prismatic Grid Regions in the SAUNA CFD CodePeace, A. J. / Chappell, J. A. / Shaw, J. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 764
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Numerical Methods for Simulating the Flow over an Airfoil Covered with a Thin Layer of LiquidBoelens, O. J. / Moeleker, P. J. J. / De Jong, H. / Hoeijmakers, H. W. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 775
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Inverse Wing Design and Optimization using the Euler Flow EquationsSedin, Y. C.-J. / Larsson, T. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 787
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Vortical Flow Simulation using an Unstructured-Grid Euler MethodRaj, P. / Kinard, T. A. / Vermeersch, S. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 798
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An Experimental Investigation into the Rationale of the Application of Wind Tunnel Wall CorrectionsAshill, P. R. / Goodyer, M. J. / Lewis, M. C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 809
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Numerical Simulation of Flowfields of the NAL Two-Dimensional Transonic Wind TunnelMatsuno, K. / Satofuka, N. / Sudani, N. / Fukuda, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 818
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Optimization of the Performance of Internal Six-Component Strain-Gage Windtunnel Balances with FEMZhai, J. N. / Ewald, B. / Hufnagel, K. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 825
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Generalization of Data Reduction Routines for Model Attitude, Force and Moment Measurements in the Wind Tunnels of the Aeronautical Institute ZarkovoVukovic, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 834
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Complete Analytical Model to Describe the Test-Leg of Scirocco PWTDe Filippis, F. / Schettino, A. / Serpico, M. / Borrelli, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 842
-
The Effective Management of Aerospace Projects through Process ModellingBalthazor, L. R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 850
-
A Virtual RafalePechaud, J. / Rouchon, C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 858
-
An Anglo-US View of Aircraft Design EducationWhitford, R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 866
-
System Synthesis in Preliminary Aircraft Design using Statistical MethodsDeLaurentis, D. / Mavris, D. N. / Schrage, D. P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 879
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High-Capacity Subsonic Transport ProjectsFielding, J. P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 892
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On the Subsonic/Supersonic, Yawed Sinusoidal Gust over an AirfoilSoviero, P. A. O. / Resende, H. B. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 901
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European 2nd Generation Supersonic Commercial Transport AircraftGreen, P. K. / Pacull, M. / Reimers, H. D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 910
-
The Oblique Flying Wing as the New Large AircraftLi, P. / Seebass, R. / Sobieczky, H. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 924
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Aerodynamic Optimization of Supersonic Transport ConfigurationsOrlowski, M. / Hermann, U. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 931
-
Flap Systems on Supersonic Transport AircraftNicholls, K. P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 937
-
The Long Term Elevated Temperature Behaviour of Materials: A Key Issue, for the Next SSTBarbaux, Y. P. / Guedra-Desgeorges, D. / Cinquin, J. / Fournier, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 943
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The Development of a Composite Root Attachment LugCathro, R. C. / Reid, R. G. / Huston, R. J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 950
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Textile Routes to Damage Tolerant Composite Structures for Aerospace ApplicationsBackhouse, R. / Bibo, G. A. / Hogg, P. J. / Mills, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 959
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Compressive Behaviour of Composite Panels Containing Impact-Induced Damages and Holes: Experimental and Numerical AnalysisEsposito, C. / Perugini, P. / Accardo, A. F. / Ricci, F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 968
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Theoretical and Experimental Analysis of Composite Beams with Elastic CouplingsKaiser, C. / Francescatti, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 979
-
Stability and Elements Postbuckling Behaviour of Complex CompositeZamula, G. N. / Ierusalimsky, K. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 990
-
Optimization of Rotating Disks via Genetic AlgorithmScaramuzzino, F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 998
-
Design Method for Marine Propeller/Stator PropulsorsAlkan, A. D. / Yilmaz, T. / Guener, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1004
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High Performance Supersonic Aircraft Intake DesignHaque, M. N. / Ransom, E. C. P. / Self, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1015
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Life Support System for Aircraft CrewNicic, N. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1023
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ETW - Flow Quality Aspects and First Model TestsQuest, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1033
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Cryogenic Model Technology for ETWIcart, G. / Angeli, T. / Dupriez, F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1044
-
The Atmospheric Reentry Simulator in NaplesEsposito, A. / Monti, R. / Zuppardi, G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1052
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The Low Speed Tiltable Wind Tunnel SWT112Rosen, J. / Nystroem, T. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1061
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Minimum Landing-Approach Distance for a VUK-T SailplaneStefanovic, Z. / Cvetkovic, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1065
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Preliminary Design of a Solar Powered Tailless MotorgliderGuglieri, G. / Quagliotti, F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1074
-
Center-of-Gravity and Lift Coefficient Limits of a Gliding Parachute. Case StudyIosilevskii, G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1081
-
Technology Assessment with Multi-Disciplinary Aircraft Design Tools on the Next Generation Supersonic Commercial TransportVon Reith, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1087
-
Sensitivities and Integrated Aerodynamic-Structural Optimal DesignArsuffi, G. / Mastroddi, F. / Morino, L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1098
-
An Object Oriented Approach to Conceptual Aircraft Design through Component-Wise ModellingSchneegans, A. / Haberland, C. / Kokorniak, M. / Domke, B. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1106
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Vibration Alleviation of a Hingeless Helicopter Rotor Blade by State FeedbackBelo, E. M. / Marques, F. D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1115
-
Active Control on Typical Helicopter Panels by using Piezo-ActuatorsDe Vivo, L. / Concilio, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1126
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Active Vibration Suppression Concepts for Buffet Excited Vertical TailsSchweiger, J. / Simpson, J. / Sensburg, O. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1137
-
Design, Analysis and Testing of a Postbuckling Co-Cured Composite Control SurfaceScott, M. L. / Cheung, A. K. H. / Newman, P. D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1148
-
Buckling and Post-Buckling Behaviour of Composite Cylindrical ShellsBisagni, C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1156
-
Postbuckling Behaviour of Graphite/Epoxy Wing Boxes Panels under Pure TorsionRomeo, G. / Frulla, G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1167
-
Unsteady Vortex Flow Phenomena on Delta Wings at High Angles of IncidenceMabey, D. G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1177
-
Fin Unsteady Surface Pressure Evaluation Due to Buffeting Based on Measured Fluctuating VelocitiesBreitsamter, C. / Laschka, B. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1189
-
An Analysis of Vortex Breakdown Predicted by the Euler EquationsStrohmeyer, D. / Orlowski, M. / Longo, J. M. A. / Hemmel, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1201
-
Calculation of Vortex Breakdown over Delta Wing by a Vortex-Lattice MethodBoffadossi, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1211
-
Influence of Fuselage Shape on Single Fin BuffetingChesneau, T. R. / Wood, N. J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1212
-
A Brief Comparison of Powered Lift, Flying Wing and Current Technology Subsonic Civil Transport Aircraft ConceptsKehayas, N. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1222
-
Space-Planes and Launchers Aerodynamic Study with Euler and Navier-Stokes ComputationsOswald, J. / Bousquet, J. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1233
-
Large Scale Navier-Stokes Multi-Body Launch Vehicle Flowfield SimulationsWang, J. C. T. / Taylor, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1240
-
Sideslip Aerodynamics for Hytex Space VehicleSillen, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1251
-
Numerical Investigations of the Flows around Various Cruciform Wing-Body Configurations at Mach Numbers from 2. to 10. and Arbitrary Angles of Attack using Sychev's TheoryVoevodenko, N. V. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1261
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Use of Neural Networks for Manoeuvre Load ControlMcLean, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1272
-
Aileron to Rudder Interconnection with Analytical RedundancyOliva, A. P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1281
-
Helicopter Inverse Simulation Incorporating an Individual Blade Rotor ModelRutherford, S. / Thomson, D. G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1294
-
Development and Trials of an Autonomous Flight Control System for UAV'sValentinis, F. / Bil, C. / Riseborough, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1304
-
Analytical-Computational Method for Matching Optimal Control FormulationsPonzi, C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1321
-
Aerodynamic Design and Technology Concepts for a New Ultra-High Capacity AircraftGreff, E. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1338
-
The Application of the Wing Tip Lifting Surfaces for Practical AerodynamicKravchenko, S. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1349
-
A Unified Boundary Integral Formulation for Acoustoaeroelastic Analysis of ShellsIemma, U. / Gennaretti, M. / Trainelli, L. / Morino, L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1355
-
Investigation into the Applicability of Neural Network to Load IdentificationCao, X. / Mitsui, Y. / Sugiyama, Y. / Tang, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1361
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Experiences with the Evaluation of the High Modal Density Structural DynamicsDe Rosa, S. / Marulo, F. / Franco, F. / Ricci, F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1367
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Scatter Factors for Damage Tolerance JustificationPizzanelli, L. / Beaufils, J. Y. / Duprat, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1375
-
On Compression Creep to Metal Matrix Composite (Al 6061) at Elevated TemperaturesIsmail, Y. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1384
-
Transient Dynamic Analysis of the Damage Process of Laminated Composite Panels and Stiffened Panels due to Low Velocity ImpactGuan, Z. D. / He, Q. Z. / Li, Z. N. / Kou, C. H. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1393
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A Probabilistic Approach to Fatigue Damage Accumulation for Damage Tolerance and Durability of Ageing AircraftLiao, M. / Xu, X. F. / Yang, Q. X. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1404
-
The New Common Mathematical Model for Expressing Fatigue Characteristics of the Typical Airframe Structure ElementsMaler, Z. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1410
-
New Nondestructive Testing Method for Ageing Evaluation of Aircraft StructurePirfo Barroso, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1414
-
The Static and Dynamic Structural Analysis of an Amphibious AircraftFaria, S. C. / Canale, A. C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1418
-
Dynamics of One-Dimensional Structures with Designed-In DisorderSayar, M. / Demirel, M. C. / Atilgan, A. R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1426
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Adaptive Local Grid Refinement for Multiblock SolversAmato, M. / Iaccarino, G. / Paparone, L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1434
-
An Improved Cebeci-Smith Turbulence Model for Boundary-Layer and Navier-Stokes MethodsCebeci, T. / Chang, K. C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1446
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Development and Application of Methods for Laminar Flow Research at ARAWong, P. W. C. / Maina, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1457
-
Viscous Coupling Techniques using Unstructured and Multiblock MeshesSzmelter, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1468
-
An Inverse-Direct Hybrid Navier-Stokes Solver using Pseude-Analytic FunctionsMiyazaki, T. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1479
-
Requirements for Effective High Lift CFDLynch, F. T. / Potter, R. C. / Spaid, F. W. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1493
-
Modelling of Flow Past Body with Thick Wake in Classical Air Wing TheoryToison, F. / Legallais, P. / Hureau, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1502
-
Aerodynamic Shape Optimization Based on High-Level PhysicsLee, K. D. / Eyi, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1513
-
Drag Reduction for Supercritical AerofoilsSedaghat, A. / Shahpar, S. / Hall, I. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1522
-
Numerical Simulation of In-Flight Aircraft IcingBrahimi, M. T. / Tran, P. / Tezok, F. / Paraschivoiu, I. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1533
-
Prediction of LE and TE Devices Aerodynamics in High-Lift Configurations with Mach and Reynolds Number EffectsNangia, R. K. / Galpin, S. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1540
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Analysis of Aircraft Maximum Performances on Optimal TrajectoriesAvanzini, G. / De Matteis, G. / De Socio, L. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1547
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Modelling of Aeroplane Dynamics in Extreme Flight ConditionsSibilski, C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1558
-
Optimal Trajectory Analysis of High Angle of Attack MissilesInnocenti, M. / Nasuti, F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1566
-
Method of Control of a Straked Wing Aircraft for Cobra ManoeuvresDzygadlo, Z. / Kowaleczko, G. / Sibilski, K. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1574
-
Tactical Utility of the X-31A Using Post Stall TechnologiesGuetter, R. / Friehmelt, H. / Haiplik, R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1584
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Numerical and Experimental Analysis of the Effect of a Pusher Propeller on a WingCatalano, F. M. / Maunsell, M. G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1595
-
Scaling of ASTOVL: Jet Flow-FieldsKnowles, K. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1606
-
Navier-Stokes Analysis for Engine Airframe IntegrationChaput, E. / Barrera, L. / Gacherieu, C. / Tourrette, L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1619
-
Afterbodies and Nozzles Optimization by using Inverse MethodsLarocca, F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1626
-
On the Numerical Investigation of Inlet Buzz FlowLu, P.-J. / Jain, L.-T. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1640
-
Airborne Systems Technology Application to the Windshear ThreatArbuckle, P. D. / Lewis, M. S. / Hinton, D. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1651
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Parametric Study of Performance of Aircraft Equipped with Airborne Reactive and Forward Looking Sensor during Microburst Encounter including Raining EffectDescatoire, F. / Guffond, D. / Huynh, H. T. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1664
-
Electromagnetic Energy for the Prevention of Ice Deposition on Aircraft SurfacesVan Loock, W. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1667
-
Flight Tests with Computer Generated Synthetic Vision for Improving Poor Visibility OperationsSachs, G. / Dobler, K. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1675
-
S.S.T.O. & T.S.T.O. LOX Collection System Performances: Influence of LOX Plant ArchitectureHendrick, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1685
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Computer-Aided Implementation of the "Duel" Airborne Operationally Consulting Expert System Investigative PrototypeRomanova, V. D. / Fedunov, B. E. / Iunevich, N. D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1692
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Optimization of Regional Aircraft Configurations from Passengers' PerspectivePant, R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1703
-
Conceptual Design Methodologies for Flyingboats and FloatplanesChicken, H. S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1715
-
Conceptual Design of an Aircraft for Australian Outback ConditionsRoots, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1726
-
Redesign and Construction of a High Performance Single Engine AeroplaneWaterhouse, J. R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1730
-
ATR/Vehicle IntegrationChristensen, K. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1741
-
Helicopter Rotor Blade Aeroacoustics: A Comparison of Model-Scale Wind Tunnel with Full-Scale Flight Test ResultsHeller, H. / Buchholz, H. / Schultz, K.-J. / Ahmed, S. R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1758
-
Investigation of the Airflow around Aircraft Model at High and Intermediate Angle of Attack with Pressure Sensitive PaintBykov, A. P. / Fonov, S. D. / Mosharov, V. E. / Orlov, A. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1768
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Static and Forced Oscillation Tests on a Generic Combat Aircraft ModelO'Leary, C. O. / Weir, B. / Walker, J. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1779
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A Transonic Doublet Lattice Method for General ConfigurationsVan Zyl, L. H. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1786
-
Further Refinement of the Nonplanar Aspects of the Subsonic Doublet-Lattice Lifting Surface MethodRodden, W. P. / Taylor, P. F. / McIntosh, S. C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1800
-
Unsteady Airloads Prediction for Oscillating Airfoils at Separated Flow ConditionsCoiro, D. P. / Pagano, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1810
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The Untied States Air Force's Use of In-Flight Simulation for Aeronautical ResearchMarkman, S. R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1818
-
The Use of Simulation Tools in the Calculation of Aircraft-Ship Interface Operational LimitsDe Ferrier, B. / Le Bihan, O. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1829
-
Some Results of Piloted Simulator Investigations on Windshear Detection Systems and Icon Display ConceptsRouwhorst, W. F. J. A. / Haverdings, H. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1856
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The Technical Development and Importance of Aircraft Recording Systems for Air Safety InvestigationMayes, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1866
-
Failure Analysis and System Designing with Reliability and Safety taken into ConsiderationBorgon, J. / Jazwinski, J. / Woropay, M. / Zurek, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1871
-
Simple Analysis to Assess the Evacuation of Transport AirplanesMartinez-Val, R. / Hernandez, C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1879
-
An Evaluation of Approach and Landing Factors Influencing Airport SafetyKhatwa, R. / Roelen, A. L. / Karwal, A. K. / Enders, J. H. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1890
-
On the Optimal Placement of PZT Actuators for the Control of the Dynamic Response of a BeamBarboni, R. / Fantini, E. / Gaudenzi, P. / Mannini, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1901
-
Vibration and Shape Control of Smart StructuresHuang, P.-Z. / Yang, S.-M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1907
-
Model-Independent Fuzzy Vibration Suppression of Flexible Structures using Non-Collocated TransducersCohen, K. / Weller, T. / Ben-Asher, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1917
-
The Robust Fault Diagnosis Based on the Singular Value DecompositionHu, C. H. / Xu, H. L. / Qing, W. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1921
-
Auto-Pilot Command-Generator Tracker Design by LEQG/LTR MethodTsai, H.-L. / Lin, J.-M. / Chang, C.-H. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1930
-
Numerical Simulation of the Performance of Aerobatic AircraftCsapo, G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1939
-
Eduction of Turbulent Structures in a Thermal Boundary Layer FlowIuso, G. / Onorato, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1947
-
Investigation into the Mixing Layer due to Two Parallel Supersonic StreamsTarnopolsky, A. Z. / Gai, S. L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1957
-
Unsteady Base Flow - Vortex Shedding and Pressure Fluctuations -Vassilopoulos, K. / Gai, S. L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1968
-
The Effect of Offset Ratio on the Mean Flow Characteristics of Turbulent Offset JetsNasr, A. / Lai, J. C. S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1979
-
Momentum and Heat Transfer in Laminar Boundary Layer Flows of Non-Newtonian Power-Law Fluids Past External SurfacesErim, M. Z. / Yuekselen, M. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 1990
-
Experimental Studies on Atomization, Vaporization and Combustion for Liquid Rocket PropulsionBrummund, U. / Cessou, A. / Vogel, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2000
-
Application of a Domain Decomposition Technique to the Mathematical Modelling of a Solid Fuel Combustion Chamber of a RamjetCoelho, P. J. / Duic, N. / Carvalho, M. G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2008
-
Possibilities of Suppression Toxic Substances Emission by Non-Stationary CombustionBazarov, V. G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2014
-
Status and Trends of Aeroengine Pollutant EmissionsHourmouziadis, J. / Wulff, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2029
-
Calculation of Turbulent Reacting Flows in a Cylindrical Combustor with Swirling InflowsBai, X.-S. / Fuchs, L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2036
-
Information Processing Strategies in Air Traffic ControllersAmaldi, P. / Boudes, N. / Cellier, J.-M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2046
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The Flight Management System within World-Wide Communication/Navigation/Surveillance and Air Traffic Management ApplicationsWittig, T. / Dudek, H.-L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2057
-
4D ATM Cockpit: Set-Up and Initial EvaluationHoogeboom, P. J. / Huisman, H. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2065
-
An Optimal Aircraft Conflict Resolution System Based on Hybrid ModelsBousson, K. / Paglione, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2081
-
Influence of Structural Modifications on the Aeroelastic Analysis of Large Transport AircraftBalis Crema, L. / Mastroddi, F. / Coppotelli, G. / Iazzetta, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2090
-
Robust Stabilization of a Transonic Flutter based on a Linearized Transonic Math ModelMatsushita, H. / Saitoh, K. / Hashidate, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2099
-
Largely Bent Wing FlutterAvertchenkov, V. V. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2110
-
The Effects of Surface Corrosion on the Fatigue Behaviour of Aluminium Alloy Specimens Containing Cold Expanded HolesGlinos, N. / Wagstaff, P. G. / Cook, R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2121
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Effect of Material Properties and Load Parameters on the Crack Growth PropagationBehal, J. / Dlouha, J. / Ruzek, R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2125
-
A Theoretical Approach for the Damage Behaviour Characterisation of Composite ShellsIkonomopoulos, G. / Perreux, D. / Marchetti, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2135
-
Studies on the Durability of Polymeric Materials for High Performance CompositesGrayson, M. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2142
-
The Prediction of Defects of A/C PressingCalkovsky, A. / Samek, R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2148
-
A Comparative Evaluation of Damage Influence on Aircraft Structure SafetyDanilecki, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2152
-
Experimental Study of Aircraft Stability Enhancement at High Angles of AttackHuang, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2162
-
Calculation of Aerodynamic Coefficients of Missile Like Geometries by Viscous/Inviscid CouplingOenen, C. / Yavuz, I. / Kavsaoglu, M. S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2171
-
Method for the Evaluation Vertical Tail Surfaces of a Light Aircraft Based on Lateral Flying QualitiesMemon, G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2177
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Steeper ApproachesRhodes, D. P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2184
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A Pure Vortex Method for Simulating Unsteady, Incompressible, Separated Flows Around Static and Pitching AerofoilsLin, H. Q. / Vezza, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2194
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Application of Viscous-Inviscid Interaction Methods for a Separated Flow Calculation about Airfoils and High-Lift SystemsLyapunov, S. V. / Wolkov, A. V. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2203
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An Accurate and Efficient Viscous Interaction Approach for Analysis and Design of Airfoils and High-Lift ConfigurationsVerhoff, A. / Michal, T. / Cebeci, T. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2214
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Convective Discretization Dependence on the Performance of Several Turbulence Models for Airfoil Stall FlowKobayashi, M. H. / Marques, N. P. C. / Pereira, J. C. F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2221
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Calculation of High-Lift Aerodynamics on Adaptive Unstructured GridsJahangirian, A. R. / Johnston, L. J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2232
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A Block Structured Based Method for the Flow Prediction over Low Reynolds Number Multi-Element AirfoilsWilquem, F. / Passelecq, C. / Degrez, G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2242
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Linear Control of Side Forces and Yawing Moments using the Dynamic Manipulation of Forebody VorticesLee, R. / Hanff, E. S. / Kind, R. J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2252
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Behaviours of Leading-Edge Separation Vortex Formed on a Delta Wing with Vortex FlapsRinoie, K. / Fujita, T. / Iwasaki, A. / Fujieda, H. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2260
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Effect of Forebody Form on the Aerodynamic Charateristics and Airflow, around an Aircraft Model up to High Angles of IncidencePesetsky, V. / Kalashnikov, S. / Lovell, D. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2271
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Effect of Lateral Blowing on Aerodynamic Characteristics of Low Aspect-Ratio Wings at High Angles of AttackKarashima, K. / Sato, K. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2278
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Aerodynamic Characteristics of a Highly Swept Wing in Steady/Unsteady Pitching States and Effects of Flap Control at Large IncidenceHsing, T. D. / Yu, G. Z. / Gu, Z. F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2289
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Experimental Measurement on Airfoils with Trailing Edge WedgesSardjadi, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2295
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Study of a Local Surface Micro-Disturbance Effects on the Supercritical Airfoil PerformanceKania, W. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2303
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WING-GRID, A Novel Device for Reduction of Induced Drag on WingsLa Roche, U. / Palffy, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2310
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Computer-Aided Engineering for the Design of Flight Control and Hydraulic SystemsScholz, D. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2320
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Effects of Anomalies in Hydraulic Actuators into Dynamics of the Aircraft Control SystemsRohacs, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2326
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A Critical Comparison between Different Methods of Flap Systems Actuation Speed LimitationBorello, L. / Villero, G. / D'Onofrio, E. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2335
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About Aeroservoelasticity Criteria for Electrohydraulic Servomechanisms SynthesisUrsu, I. / Vladimirescu, M. / Ursu, F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2345
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Computer Analysis and Simulation of Transient State and Pressure Recovering in Fast Cyclic Hydraulic ActuatorsJankovic, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2356
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Digital Redesign of the NRC Bell 205 Artificial Feel SystemGubbels, A. W. / Goheen, K. R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2366
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Numerical Study of Aerodynamic High Speed Propeller Engine Integration on Transport AircraftColin, P. / Moreux, V. / Barillier, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2381
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Experimental Investigation on Propeller Slipstream Interference Effects on a Swept Wing at Low Speed ConditionsPrijo Kusumo, J. / Gayus, N. / Custers, L. G. M. / De Haij, L. H. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2392
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Analysis of Propeller Slipstream Effects on a Trailing WingVeldhuis, L. L. M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2414
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Measurements of the Propeller Slipstream Interaction with a Nacelle and WingBarber, D. J. / Nelson, T. E. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2425
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Analysis of Propeller Slipstream FieldWang, D. Q. / Lindblad, I. / Eliasson, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2434
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Nonlinear Vibration Tests of Isotropic Cylindrical Shells under Comprehensive Axial LoadsGunawan, L. / Klompe, A. W. H. / Zwaan, R. J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2445
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Behaviour of an Aeronautic Composite Panel submitted to an Impulsive LoadingMoreno, A. / Dauce, J.-P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2451
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Vibrations and Stability of a Biself-Excited Surface Structure in Supersonic Flow Subjected to a Follower ForceDzygadlo, Z. / Nowotarski, I. / Olejnik, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2461
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Effects of Replacement of a Dynamic Crash Test with a Quasi Dynamic One. Test of the PW-5 World Class GliderCzarnocki, P. / Wiacek, T. / Wingralek, W. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2465
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The Application of Dynamic Loads to a Full Scale F/A-18 Fatigue Test ArticleConser, D. P. / Graham, A. D. / Smith, C. J. / Yule, C. L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2481
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The Interaction between Secondary Flow and Film Cooling in a Turbine NozzleLangowsky, C. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2490
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The Influence of Rotation and Buoyancy on Radially Inward and Outward Directed Flow in a Rotating Circular Coolant ChannelElfert, M. / Hoevel, H. / Towfighi, K. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2501
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Flow Separation Prediction on Inlets with Mach and Reynolds Number Effects in Subsonic FlightNangia, R. K. / Palmer, M. E. / Hodges, J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2511
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Validation of Non-Axisymmetric Terms in 3-D Viscous Flow Analysis for High Speed Axial CompressorsKaldellis, J. K. / Georgantopoulos, G. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2522
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Heat Transfer around a 180deg Turn in a Square ChannelCarlomagno, G. M. / Cardone, G. / Astarita, T. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2528
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Analysis of Wrap-Around Finned Missiles with a Zonal Navier-Stokes SolverSen, T. S. / Korkem, B. / Temel, B. / Kavsaoglu, M. S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2538
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Aerodynamic Design of Swept Infinite Wing with Flap for Subsonic and Transonic Flight RegimesKovalev, K. V. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2549
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Aircraft Induced Drag Minimization Using the Constrained Optimization MethodMartins, A. L. / Ribeiro, R. S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2558
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Numerical Solution of Axisymmetric Jet-Plume Coupled with External FreestreamYilmaz, E. / Kavasaoglu, M. S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2565
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Developed CAI Model for Complex PartsZivkovic, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2571
-
Navier-Stokes Calculations for a Complete AircraftLehtimaeki, R. / Laine, S. / Siikonen, T. / Salminen, E. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2579
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Joined-Wing Configuration AerodynamicsWai, J. C. / Herling, W. W. / Roetman, E. L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2590
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Investigation of the Vortex Wake Evolution and Flight SafetyVyshinsky, V. V. / Soudakov, G. G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2601
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The Unsteady Pressure Field on a Wing with Large Regions of Separated FlowLee, B. H. K. / Marineau-Mes, S. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2611
-
Unsteady Aerodynamic Phenomena on Novel Wing PlanformsWoods, M. I. / Wood, N. J. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2622
-
The Comparison between the Dynamic Stall of a Finite Wing with Straight and Swept TipsGalbraith, R. A. M. / Coton, F. N. / Jiang, D. / Gilmour, R. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2634
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Rate Limiters with Phase CompensationRundqwist, L. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2643
-
Robust Autopilot Design Strategy for Functionally Dependent Parameter UncertaintiesShaviv, G. E. / Idan, M. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2653
-
In-Flight Monitoring of Critical SensorsJann, T. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2659
-
Landing Gear Integration on a Supersonic Transport AircraftRoloff, G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2667
-
Semi-Active Controlled Shock Absorber for Large Flexible AircraftWentscher, H. / Roloff, G. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2678
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The Simulation of Aircraft Landing Gears During Usual and Unusual ManoeuvresKapadoukas, G. G. / Self, A. W. / Marteau, F. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2689
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Well-Conditioned Procedures for Optimal Robust Design of Flight Control SystemsStoica, A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2699
-
Buckling Behaviour of Large GLARE Fuselage Shells under Compression and Shear LoadingHorst, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2710
-
Postbuckling of Laminated Composite and Sandwich-Type Plates and Shells: On the Significance of the Fulfillment of Static Interlayer Continuity ConditionsLibrescu, L. / Lin, W. / DiSciuva, M. / Icardi, U. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
- 2722
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Application of Skew-Transversely-Repetitive Analysis for Buckling of Plate Arrays with Curved or Straight Internal SupportsYork, C. B. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996
-
Conceptual Design for Passenger Airplane of Very Large Passenger Capacity in Flying Wing LayoutDenisov, V. E. / Bolsunovsky, A. L. / Buzoverya, N. P. / Gurevich, B. I. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences et al. | 1996