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209 items

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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): Gregorek, G. M., Nark, T. C., Lee, J. D.
Corporate Author(s): Ohio State University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-03
Report number: ASD TDR 62-792 Volume 2
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NB-66B High Altitude Gust Survey Technical Analysis, Volume I.
Author(s): Strom, J. A., Weathermon, T. G.
Corporate Author(s): Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-04
Report number: ASD TDR 63-145 Volume 1
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NB-66B High Altitude Gust Survey Power Spectra, Volume II.
Author(s): Strom, J. A., Weathermon, T. G.
Corporate Author(s): Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-04
Report number: ASD TDR 63-145 Volume 2
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NB-66B High Altitude Gust Survey Time Series, Volume III.
Author(s): Strom, J. A., Weathermon, T. G.
Corporate Author(s): Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-04
Report number: ASD TDR 63-145 Volume 3
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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, Amey, Harry B., Jr.
Corporate Author(s): 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, Malvestuto, Frank S., Stuart, Jay W.
Corporate Author(s): Lockheed-California Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-04
Report number: ASD TR 61-433 Volume 1
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Application Of The Subdomain (Biezeno-Koch) Method To Circular Plate Bending
Author(s): Adams, O. E., Jr
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1967-06
Report number: AFFDL TR 66-215
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Measurement Of The Diffraction Correction Of The Gulton Model P420m-6 Microphone
Author(s): Ortega, Jose C.
Corporate Author(s): Western Electro-Acoustic Lab Inc Santa Monica CA
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1967-05
Report number: AFFDL TR 66-223
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The Evolution of USAF Environmental Testing
Author(s): Junker, V. J.
Corporate Author(s): Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1965-10
Report number: AFFDL TR 65-197
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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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