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209 items

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Six-Degree-Of-Freedom Flight-Path Study Generalized Computer Program: Part II User's Manual
Author(s): Seubert, Frederick W., Usher, Newell E.
Corporate Author(s): 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, Tan Hsu, Pao
Corporate Author(s): 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(s): 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(s): 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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Measurement and Analysis of Power Spectra and Cross-Power Spectra for Random Phenomena
Author(s): Bendat, Julius S.
Corporate Author(s): Thompson Ramo-Wooldrige Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1960-10
Report number: WADD TR 60-681
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Feasibility To Determine Practicability Of Providing Mockup Improvements
Author(s): Lowe, W. F., Calvin, C. C., Doughty, L. E.
Corporate Author(s): 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., Watanabe, Roy K.
Corporate Author(s): 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., Young, Kenneth J., Sutherland, L. C.
Corporate Author(s): The Acoustics Group, Aero-Space Division, Boeing Airplane Company
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-04
Report number: WADD TR 61-178
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Automatic Runway Profile Measuring Instrumentation And Runway Properties. Part II: Equipment Trials
Author(s): Turner, D. F., Brown, R. S., Patton, P. C.
Corporate Author(s): Midwest Research Institute
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-10
Report number: WADD TR 60-470 Part II
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Multiwall Structures For Space Vehicles
Author(s): Lampert, S., Younger, D. G.
Corporate Author(s): 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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