27 reports
Application of the NASA Kernel-Function Procedures to Generally Deforming Wings
Author(s): None Given Corporate Author: Aerojet-General Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-10 Report Number: ASD TDR 62-409
Track Tests Of Canopy Escape Capsule
Author(s): Lubinski, Thomas P. Corporate Author: Coleman Engineering Co Inc Torrance Calif Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-08 Report Number: ASD TDR 62-404
Study of a Sonic Load Recorder, Volume I.
Author(s): Ball, Jay H. Corporate Author: Bolt Beranek and Newman Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-11 Report Number: ASD TDR 62-165 Volume 1
Structural Flight Loads Data from F-106A Aircraft
Author(s): Vahldiek, Artie Corporate Author: Flight Dynamics Laboratory Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-02 Report Number: ASD TDR 62-246
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Lift, Pitching-Moment, and Rolling-Moment Coefficients on Planar, Twisted, and Cambered Wings and Flaps for a 70 Degree Delta Wing: Part Two - Transonic Flow
Author(s): Mazelsky, Bernard Corporate Author: Aeroject-General Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-11 Report Number: ASD TDR 62-155 Part 2
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Further Studies on High-Speed Unsteady Flow
Author(s): Zartanian, Garabed Corporate Author: Massachusetts Institute of Technology Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-09 Report Number: ASD TDR 62-463
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Advanced Concepts of Stochastic Processes and Statistics for Flight Vehicle Vibration Estimation and Measurement
Author(s): Bendat, Julius S. Corporate Author: Thompson Ramo Wooldrige, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-12 Report Number: ASD TDR 62-973
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Investigation of Stabilization and Control Systems for Application to Aero Space Vehicle Escape Capsules
Author(s): Chew, F. E. Corporate Author: Chance Vought Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-06 Report Number: ASD TDR 62-243
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Optimum Fatigue Spectra
Author(s): Neuls, G. S. Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-03 Report Number: WADD TR 60-398
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Strength, Efficiency, and Design Data for Beryllium Structures
Author(s): Crawford, Robert F. Corporate Author: Lockheed Missiles & Space Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-02 Report Number: ASD TR 61-692
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On Developing a Low Altitude Turbulence Model for Aircraft Gust Loads
Author(s): Lappe, U. O. Corporate Author: New York University Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-06 Report Number: ASD TDR 62-152
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Optimum Fatigue Spectra
Author(s): Neuls, G. S. Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-04 Report Number: ASD TR 61-235
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Establishment of the Approach to, and Development of, Interim Design Criteria for Sonic Fatigue
Author(s): Fitch, G. E. Corporate Author: North American Aviation, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-06 Report Number: ASD TDR 62-26 AD Number: AD0284597
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Research on Techniques of Establishing Random Type Fatigue Curves for Broad Band Sonic Loading
Author(s): Fuller, J. R. Corporate Author: The Boeing Company, Transport Division Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-10 Report Number: ASD TDR 62-501
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Practical Aspects of Aerothermoelastic Modelling
Author(s): Schlessinger, M. Corporate Author: Flight Sciences Laboratory, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-12 Report Number: ASD TDR 62-705
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New Approaches to Flight Vehicle Structural Vibration Analysis and Control
Author(s): Heck, Manfred A. Corporate Author: Bolt, Beranek & Newman, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-10 Report Number: ASD TDR 62-237
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Uniform Heating Effects on the Response of a High Speed Vehical to Discrete and Continuous Gusts
Author(s): Peboulet, R. P. Corporate Author: General Dynamics Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-04 Report Number: ASD TR 61-328
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Inspection Periods Determined from Data of Crack Development and Strength Reduction of an Aircraft Structure Using Static Analysis
Author(s): Eggwertz, Sigge Corporate Author: The Aeronautical Research Institute of Sweden (FFA) Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-05 Report Number: ASD TDR 62-391
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An Engineering Evaluation of Methods for the Prediction of Fatigue Life in Airframe Structures
Author(s): Crichlow, W. J. Corporate Author: Lockheed Aircraft Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-03 Report Number: ASD TR 61-434
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Study to Determin Skin-Friction Drag in Hypersonic Low-Density Flow: Vlume I: Summary Analysis
Author(s): Francis, W. Leon Corporate Author: Lockheed-California Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-04 Report Number: ASD TR 61-433 Volume 1
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Survey and Evaluation of Sonic Fatigue Testing Facilities
Author(s): Bianchi, Ralph A. Corporate Author: CONESCO Consultants in Engineering Science Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-03 Report Number: ASD TR 61-185 AD Number: AD0277124
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Thermo-Structural Analysis Manual
Author(s): Forray, M. J. Corporate Author: Republic Aviation Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-10 Report Number: WADD TR 60-517 Vol II
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Shock-Tube Measurements of Step-Blast Loads on a NASA 64A010 Airfoil
Author(s): Ruetenik, J. Ray Corporate Author: Massachusetts Institute of Technology Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-02 Report Number: ASD TR 61-219
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Methods For Analyzing Flight Vehicles During The Taxi Condition
Author(s): Theisen, J. G. Corporate Author: Lockheed-Georgia Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-01 Report Number: ASD TR 61-177 AD Number: AD0273305
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Prediction Of Creep Effects In Aircraft Structures
Author(s): Alesch, C. W. Corporate Author: Convair, A Division of General Dynamics Corporation Engineering Department Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-02 Report Number: WADD TR 60-411 Part 2
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A Theoretical And Experimental Investigation Of The Acoustic Response Of Cavities In An Aerodynamic Flow
Author(s): Plumblee, H. E. Corporate Author: Flight Dynamics Laboratory Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-03 Report Number: WADD TR 61-75
Thermo-Structural Analysis Manual
Author(s): Switzky, H. Corporate Author: Republic Aviation Corp Farmingdale N Y Laboratory: Flight Dynamics Laboratory Date of Publication: 1962-08 Report Number: WADD TR 60-517 Volume I