201 reports
Methods of Space Vehicle Noise Prediction
Author(s): Peter A. Franken Corporate Author: Bolt Beranek and Newman Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 9/1/1960 Report Number: WADC TR 58-343 Volume 2
Similarity Studies For Dissociating Gases In Hypersonic , Low Density Flow
Author(s): K.Pearce, S.Samet And R.J.Whalen Corporate Author: Flight Sciences Laboratory, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 9/1/1960 Report Number: WADD TR 60-341
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Transient And Nonlinear Effects On High Speed. Vibratory, Thermoelastic Instability Phenomena.
Author(s): Eugene J. Brunelle, Jr. Corporate Author: Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology Laboratory: Flight Dynamics Laboratory Date of Publication: 12/1/1960 Report Number: WADD TR 60-484 Part 2
Multiwall Structures For Space Vehicles
Author(s): S. Lampert; D. G. Younger Corporate Author: Aeronutronic, A Division of Ford Motor Company Laboratory: Flight Dynamics Laboratory Date of Publication: 5/1/1960 Report Number: WADD TR 60-503
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Investigation Of Thermal Effects On Structural Fatigue
Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 8/1/1960 Report Number: WADD TR 60-410 Part 1
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Prediction Of Creep Effects In Aircraft Structures
Author(s): C. W. Alesch; C. Riparbelli; W. H. Steurer; W. Robe Corporate Author: Convair, A Division of General Dynamics Corporation Engineering Department Laboratory: Flight Dynamics Laboratory Date of Publication: 4/15/1960 Report Number: WADD TR 60-411 Part 1
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Time-Dependant, Elasto-Plastic Bending Analysis For Structures Under Arbitrary Load-Temperature Environments. Part I: Analysis Development And Digital Program
Author(s): P. C. Huang Corporate Author: The Martin Company Laboratory: Flight Dynamics Laboratory Date of Publication: 4/1/1960 Report Number: WADD TR 60-541 Part 1
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Time-Dependant, Elasto-Plastic Bending Analysis For Structures Under Arbitrary Load-Temperature Environments. Part II: Experimental Verification
Author(s): C. J. Van Der Mass Corporate Author: The Martin Company Laboratory: Flight Dynamics Laboratory Date of Publication: 4/1/1960 Report Number: WADD TR 60-541 Part 2
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An Experimental Study On Multi-Wall Structures For Space Vehicles
Author(s): D.G. Younger, S. Lampert Corporate Author: Aeronutronic, A Division Of Ford Motor Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1/1/1961 Report Number: WADD TR 60-800
Thermo-Structural Analysis Manual
Author(s): Switzky, H.; Forray, M.J.; Newman, M. Corporate Author: Republic Aviation Corp Farmingdale N Y Laboratory: Flight Dynamics Laboratory Date of Publication: 8/1/1962 Report Number: WADD TR 60-517 Volume 1
The Dynamic Response of Advanced Vehicles
Author(s): Q. R. Bohne; B. E. Clingan; C. W. DeCeault; P. C Deutschle Corporate Author: Boeing Airplane Company Laboratory: Flight Dynamics Laboratory Date of Publication: 9/1/1960 Report Number: WADD TR 60-518
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Measurement and Analysis of Power Spectra and Cross-Power Spectra for Random Phenomena
Author(s): Julius S. Bendat Corporate Author: Thompson Ramo-Wooldrige Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 10/1/1960 Report Number: WADD TR 60-681
Feasibility To Determine Practicability Of Providing Mockup Improvements
Author(s): W. F. Lowe, C. C. Calvin, L. E. Doughty Corporate Author: Chance Vought Aircraft, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 8/1/1961 Report Number: WADD TR 60-579
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Admittance Techniques In high Speed Flutter Model Testing. Part I. Experimental Results
Author(s): Gifford W, Asher And Roy K. Watanabe Corporate Author: Boeing Company Laboratory: Flight Dynamics Laboratory Date of Publication: 7/1/1961 Report Number: WADD TR 61-31 Part 1
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The Use Of Acoustic Scale Models For Investigating Near Field Noise Of Jet And Rocket Engines
Author(s): Walter V. Morgan, L. C. Sutherland, Kenneth J. Young Corporate Author: The acoustics Group, Aero-Space Division, Boeing Airplane Company Laboratory: Flight Dynamics Laboratory Date of Publication: 4/1/1961 Report Number: WADD TR 61-178
Automatic Runway Profile Measuring Instrumentation And Runway Properties. Part II: Equipment Trials
Corporate Author: Midwest Research Institute Laboratory: Flight Dynamics Laboratory Date of Publication: 10/1/1961 Report Number: WADD TR 60-470 Part 2
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A Study Of The Characteristics O Fmodern Engine Noise And The Response Characteristics Of Structures
Author(s): R. J. Cox, H. J. Parry, J. Clough Corporate Author: Lockheed Aircraft Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 12/1/1961 Report Number: WADD TR 60-220
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Investigation Of Escape Capsule Systems For Multi-place Aircraft . Part I: Preliminary Investigation
Author(s): J. J. Vorachek; F. Milhoan Corporate Author: Goodyear Aircraft Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 12/1/1961 Report Number: WADC TR 57-329 Part 1
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Investigation Of Escape Capsule Systems For Multi-place Aircraft. Part II: Preliminary Design And wind Tunnel Testing Of An Individual Escape Capsule
Author(s): F. M. Milhoan; J. J. Vorachek; J. D'Allura Corporate Author: Goodyear Aircraft Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 12/1/1961 Report Number: WADC TR 57-329 Part 2
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Automatic Runway Profile Measuring Instrumentation And Runway Properties. Part I: Equipment
Author(s): D. F. Turner, R. S. Brown, W. E. Snyder Corporate Author: Midwest Research Institute Laboratory: Flight Dynamics Laboratory Date of Publication: 2/1/1961 Report Number: WADD TR 60-470 Part 1
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Investigation Of Thermal Effects On Structural Fatigue
Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 8/1/1961 Report Number: WADD TR 60-410 Part 2
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Six-Degree-Of-Freedom Flight-Path Study Generalized Computer Program
Author(s): Robert C. Brown; Robert V. Brulle; Gerald D. Giffin Corporate Author: McDonnell Aircraft Corporation, St. Louis, Missouri Laboratory: Flight Dynamics Laboratory Date of Publication: 5/1/1961 Report Number: WADD TR 60-781 Part 1
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A Theoretical And Experimental Investigation Of The Acoustic Response Of Cavities In An Aerodynamic Flow
Author(s): H. E. Plumblee, J. S. Gibson, L. W. Lassiter Corporate Author: Flight Dynamics Laboratory Laboratory: Flight Dynamics Laboratory Date of Publication: 3/1/1962 Report Number: WADD TR 61-75
Six-Degree-Of-Freedom Flight-Path Study Generalized Computer Program: Part 2 User's Manual
Author(s): Frederick W. Seubert; Newell E. Usher Corporate Author: McDonnel Aircraft Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 5/1/1961 Report Number: WADD TR 60-781 Part 2
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Theoretical And Experimental Studies On Airloads Related To Hypersonic Aeroelastic Problems Of General Slender Pointed Configurations
Author(s): Zartarian, Garabed; Tan Hsu,Pao Corporate Author: Massachusetts Inst Of Tech Cambridge Aeroelastic And Structures Research Lab Laboratory: Flight Dynamics Laboratory Date of Publication: 4/1/1961 Report Number: ASD TR 61-7
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Structural Response Of Beryllium Sheet Produced By Three Fabrication Methods
Author(s): Giemza, C. J. Corporate Author: Martin Co Baltimore Md Laboratory: Flight Dynamics Laboratory Date of Publication: 12/1/1961 Report Number: ASD TR 61-87
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Compressible Boundary Layer Equations And Stagnation Point Solution With Differences In Thermal And Dynamic Boundary Layer Thicknesses Being Considered
Author(s): Buck,Melving L. Corporate Author: Aeronautical Systems Div Wright-Patterson AFB Ohio Flight Control Lab Laboratory: Flight Dynamics Laboratory Date of Publication: 8/1/1961 Report Number: ASD TR 61-107
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Prediction Of Creep Effects In Aircraft Structures
Author(s): C. W. Alesch, B. Klein, and W. Robe Corporate Author: Convair, A Division of General Dynamics Corporation Engineering Department Laboratory: Flight Dynamics Laboratory Date of Publication: 2/1/1962 Report Number: WADD TR 60-411 Part 2
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Methods For Analyzing Flight Vehicles During The Taxi Condition
Author(s): Theisen, J. G Corporate Author: Lockheed Aircraft Corp Marietta GA Laboratory: Flight Dynamics Laboratory Date of Publication: 1/1/1962 Report Number: ASD TR 61-177
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Study of a Sonic Load Recorder, Volume I.
Author(s): Jay H. Ball, Norman Doelling, Denis U. Noiseux, Edward A. Starr Corporate Author: Bolt Beranek and Newman Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 11/1/1962 Report Number: ASD TDR 62-165 Volume 1
Study of a Sonic Load Recorder, Volume II.
Author(s): P. W. Smith, Jr., E. A. Starr, C. W. Dietrich, D. U. Noiseux Corporate Author: Bolt Beranek and Newman Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 3/1/1963 Report Number: ASD TDR 62-165 Volume 2
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: 10/1/1962 Report Number: ASD TDR 62-409
Further Studies on High-Speed Unsteady Flow
Author(s): Garabed Zartanian; Harry Sauerwein Corporate Author: Massachusetts Institute of Technology Laboratory: Flight Dynamics Laboratory Date of Publication: 9/1/1962 Report Number: ASD TDR 62-463
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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: 8/1/1962 Report Number: ASD TDR 62-404
Structural Flight Loads Data from F-106A Aircraft
Author(s): Artie Vahldiek; John B. Monfort Corporate Author: Flight Dynamics Laboratory Laboratory: Flight Dynamics Laboratory Date of Publication: 2/1/1962 Report Number: ASD TDR 62-246
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Investigation of Stabilization and Control Systems for Application to Aero Space Vehicle Escape Capsules
Author(s): F. E. Chew; L. Oling; H. A. Clutz Corporate Author: Chance Vought Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 6/1/1962 Report Number: ASD TDR 62-243
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Practical Aspects of Aerothermoelastic Modelling
Author(s): M. Schlessinger; B. Omilian; J. Deutschman; J. S. Isenberg Corporate Author: Flight Sciences Laboratory, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 12/1/1962 Report Number: ASD TDR 62-705
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Uniform Heating Effects on the Response of a High Speed Vehical to Discrete and Continuous Gusts
Author(s): R. P. Peboulet; P. G. Warner Corporate Author: General Dynamics Laboratory: Flight Dynamics Laboratory Date of Publication: 4/1/1962 Report Number: ASD TR 61-328
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Shock-Tube Measurements of Step-Blast Loads on a NASA 64A010 Airfoil
Author(s): J. Ray Ruetenik; Walter Herrmann Corporate Author: Massachusetts institute of Technology Laboratory: Flight Dynamics Laboratory Date of Publication: 2/1/1962 Report Number: ASD TR 61-219
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On Developing a Low Altitude Turbulence Model for Aircraft Gust Loads
Author(s): U. O. Lappe; J. Clodman Corporate Author: New York University Laboratory: Flight Dynamics Laboratory Date of Publication: 6/1/1962 Report Number: ASD TDR 62-152
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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): Bernard Mazelsky; Harry B. Amey, Jr. Corporate Author: Aeroject-General Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 11/1/1962 Report Number: ASD TDR 62-155 Part 2
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Study to Determin Skin-Friction Drag in Hypersonic Low-Density Flow: Vlume I: Summary Analysis
Author(s): W. Leon Francis; Frank S. Malvestuto; Jay W. Stuart Corporate Author: Lockheed-California Company Laboratory: Flight Dynamics Laboratory Date of Publication: 4/1/1962 Report Number: ASD TR 61-433 Volume 1
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New Approaches to Flight Vehicle Structural Vibration Analysis and Control
Author(s): Manfred A. Heckl; Richard H. Lyon; Gideon Maidanik; Eric E. Ungar Corporate Author: Bolt, Beranek & Newman, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 10/1/1962 Report Number: ASD TDR 62-237
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Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure
Author(s): W. H. Roberts; P. E. Finwall; R. W. White; K. E. Eldred Corporate Author: Northup Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 8/1/1963 Report Number: ASD TDR 62-801
An Engineering Evaluation of Methods for the Prediction of Fatigue Life in Airframe Structures
Author(s): W. J. Crichlow; A. J. McCulloch Corporate Author: Lockheed Aircraft Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 3/1/1962 Report Number: ASD TR 61-434
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Advanced Concepts of Stochastic Processes and Statistics for Flight Vehicle Vibration Estimation and Measurement
Author(s): Julius S. Bendat; Loren D. Enochson; G. Harold Klein; Allan G. Piersol Corporate Author: Thompson Ramo Wooldrige, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 12/1/1962 Report Number: ASD TDR 62-973
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Optimum Fatigue Spectra
Author(s): G. S. Neuls Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 3/1/1962 Report Number: WADD TR 60-398
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Thermo-Structural Analysis Manual
Author(s): M. J. Forray; M. Newman; H. Switzky Corporate Author: Republic Aviation Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 10/1/1962 Report Number: WADD TR 60-517 Vol II
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An Experimental Investigation of the Surfact Pressure and the Laminar Boundary Layer on a Blunt Flat Plate in Hypersonic Flow: Vol. I. Surface Pressure Distributions on a Blunted Flat Plate
Author(s): G. M. Gregorek; T. C. Nark; J. D. Lee Corporate Author: Ohio State University Laboratory: Flight Dynamics Laboratory Date of Publication: 3/1/1963 Report Number: ASD TDR 62-792 Volume 1
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An Experimental Investigation of the Surfact Pressure and the Laminar Boundary Layer on a Blunt Flat Plate in Hypersonic Flow: Vol. II. Laminar Boundary Layer Profile on the Flat Plate
Author(s): G. M. Gregorek; T. C. Nark; J. D. Lee Corporate Author: Ohio State University Laboratory: Flight Dynamics Laboratory Date of Publication: 3/1/1963 Report Number: ASD TDR 62-792 Volume 2
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