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Shock-Tube Measurements of Step-Blast Loads on a NASA 64A010 Airfoil
Author(s): Ruetenik, J. Ray, Herrmann, Walter
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Report number: ASD TR 61-219
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Further Studies on High-Speed Unsteady Flow
Author(s): Zartanian, Garabed, Sauerwein, Harry
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-09
Report number: ASD TDR 62-463
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Thermo-Structural Analysis Manual
Author(s): Forray, M. J., Newman, M., Switzky, H.
Corporate Author(s): Republic Aviation Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-10
Report number: WADD TR 60-517 Vol II
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Prediction Of Creep Effects In Aircraft Structures
Author(s): Alesch, C. W., Klein, B. , Robe, W.
Corporate Author(s): 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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Methods For Analyzing Flight Vehicles During The Taxi Condition
Author(s): Theisen, J. G.
Corporate Author(s): Lockheed-Georgia Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-01
Report number: ASD TR 61-177
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Strength, Efficiency, and Design Data for Beryllium Structures
Author(s): Crawford, Robert F., Burns, A. Bruce
Corporate Author(s): Lockheed Missiles & Space Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Report number: ASD TR 61-692
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Survey and Evaluation of Sonic Fatigue Testing Facilities
Author(s): Bianchi, Ralph A., Bradshaw, Ronald T., Farrell, James H., Reed, F. Everett
Corporate Author(s): CONESCO Consultants in Engineering Science
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-03
Report number: ASD TR 61-185
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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(s): The Boeing Company, Transport Division
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-10
Report number: ASD TDR 62-501
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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(s): 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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