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209 reports
Methods of Space Vehicle Noise Prediction
Author(s): Franken, Peter A. Corporate Author: Bolt Beranek and Newman Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1960-09 Report Number: WADC TR 58-343 Volume 2
A Study Of The Characteristics O Fmodern Engine Noise And The Response Characteristics Of Structures
Author(s): Cox, R. J. Corporate Author: Lockheed Aircraft Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-12 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): Vorachek, J. J. Corporate Author: Goodyear Aircraft Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-12 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): Milhoan, F. M. Corporate Author: Goodyear Aircraft Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-12 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): Turner, D. F. Corporate Author: Midwest Research Institute Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-02 Report Number: WADD TR 60-470 Part I
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Investigation Of Thermal Effects On Structural Fatigue
Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-08 Report Number: WADD TR 60-410 Part 2
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Six-Degree-Of-Freedom Flight-Path Study Generalized Computer Program
Author(s): Brown, Robert C. Corporate Author: McDonnell Aircraft Corporation, St. Louis, Missouri Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-05 Report Number: WADD TR 60-781 Part I
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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
Multiwall Structures For Space Vehicles
Author(s): Lampert, S. Corporate Author: Aeronutronic, A Division of Ford Motor Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1960-05 Report Number: WADD TR 60-503
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Transient And Nonlinear Effects On High Speed, Vibratory, Thermoelastic Instability Phenomena. Part II Aerothermoelastic Applications
Author(s): Brunelle, Eugene J., Jr. Corporate Author: Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology Laboratory: Flight Dynamics Laboratory Date of Publication: 1960-12 Report Number: WADD TR 60-484 Part II
Measurement and Analysis of Power Spectra and Cross-Power Spectra for Random Phenomena
Author(s): Bendat, Julius S. Corporate Author: Thompson Ramo-Wooldrige Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1960-10 Report Number: WADD TR 60-681
Feasibility To Determine Practicability Of Providing Mockup Improvements
Author(s): Lowe, W. F. Corporate Author: Chance Vought Aircraft, Incorporated Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-08 Report Number: WADD TR 60-579
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Admittance Techniques In high Speed Flutter Model Testing. Part I. Experimental Results
Author(s): Asher, Gifford W. Corporate Author: Boeing Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-07 Report Number: WADD TR 61-31 Part I
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The Use Of Acoustic Scale Models For Investigating Near Field Noise Of Jet And Rocket Engines
Author(s): Morgan, Walter V. Corporate Author: The Acoustics Group, Aero-Space Division, Boeing Airplane Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-04 Report Number: WADD TR 61-178
Automatic Runway Profile Measuring Instrumentation And Runway Properties. Part II: Equipment Trials
Author(s): Turner, D. F. Corporate Author: Midwest Research Institute Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-10 Report Number: WADD TR 60-470 Part II
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Similarity Studies For Dissociating Gases In Hypersonic , Low Density Flow
Author(s): Pearce, K. Corporate Author: Flight Sciences Laboratory, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1960-09 Report Number: WADD TR 60-341
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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
The Dynamic Response of Advanced Vehicles
Author(s): Bohne, Q. R. Corporate Author: Boeing Airplane Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1960-09 Report Number: WADD TR 60-518
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Investigation Of Thermal Effects On Structural Fatigue
Corporate Author: Douglas Aircraft Company, Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1960-08 Report Number: WADD TR 60-410 Part 1
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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: 1960-04-15 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): Huang, P. C. Corporate Author: The Martin Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1960-04 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): Van Der Maas, C. J. Corporate Author: The Martin Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1960-04 Report Number: WADD TR 60-541 Part II
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An Experimental Study On Multi-Wall Structures For Space Vehicles
Author(s): Younger, D. G. Corporate Author: Aeronutronic, A Division Of Ford Motor Company Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-01 Report Number: WADD TR 60-800
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
Study of a Sonic Load Recorder, Volume II.
Author(s): Smith, P. W., Jr. Corporate Author: Bolt Beranek and Newman Inc. Laboratory: Flight Dynamics Laboratory Date of Publication: 1963-03 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: 1962-10 Report Number: ASD TDR 62-409
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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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
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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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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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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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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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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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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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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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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Six-Degree-Of-Freedom Flight-Path Study Generalized Computer Program: Part II User's Manual
Author(s): Seubert, Frederick W. Corporate Author: McDonnel Aircraft Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-05 Report Number: WADD TR 60-781 Part II
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Theoretical And Experimental Studies On Airloads Related To Hypersonic Aeroelastic Problems Of General Slender Pointed Configurations
Author(s): Zartarian, Garabed Corporate Author: Massachusetts Institute of Technology Laboratory: Flight Dynamics Laboratory Date of Publication: 1961-04 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: 1961-12 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: 1961-08 Report Number: ASD TR 61-107
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Response of Missile Structures to Impulse Loading
Author(s): Wah, T. Corporate Author: Southwest Research Institute Laboratory: Flight Dynamics Laboratory Date of Publication: 1963-03 Report Number: ASD TDR 62-475
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Investigation of Stored Energy Rotors for Recovery
Author(s): Robinson, D. W., Jr. Corporate Author: Kaman Aircraft Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1963-12 Report Number: ASD-TDR-63-745 AD Number: AD0428998
Feasibility Studies on Use of Artrons as Logic Elements in Flight Control Systems
Author(s): Mirabelli, R. E. Corporate Author: Flight Dynamics Laboratory Laboratory: Flight Dynamics Laboratory Date of Publication: 1964-09 Report Number: FDL TDR 64-23
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Stagnation Point Heat Transfer in High Enthalpy Gas Flows, Part I: Convective Heat Transfer in Partially Ionized Air
Author(s): Nerem, Robert M. Corporate Author: Ohio State University Laboratory: Flight Dynamics Laboratory Date of Publication: 1964-03 Report Number: FDL TDR 64-41 Part 1
Stagnation Point Heat Transfer in High Enthalpy Gas Flows, Part II: Shock Layer Radiative Emission During Hypervelocity Re-Entry
Author(s): Nerem, Robert M. Corporate Author: Ohio State University Laboratory: Flight Dynamics Laboratory Date of Publication: 1964-03 Report Number: FDL TDR 64-41 Part 2
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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Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure
Author(s): Roberts, W. H. Corporate Author: Northup Corporation Laboratory: Flight Dynamics Laboratory Date of Publication: 1963-08 Report Number: ASD TDR 62-801
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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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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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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