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A Technique for Measuring In-Plane Displacements By Holographic Interferometry
Author(s): Adams, Frank D., Corwin, Richard R.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-02
Report number: AFFDL TR 72-5
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Test of the Air Cushion Landing System on the XC-8A
Author(s): Buzzard, Wallace C., Perez, David J., Wyen, Gerald, Randall, John
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1978-04
Report number: AFFDL TR 78-61
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Laboratory Tests of an Air Cushion Recovery System for the Jindivik Aircraft
Author(s): Vaughan, John C., III, Steiger, James T., Pool, David J., Campbell, Shade
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1974-04
Report number: AFFDL TR 74-64
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Ejector Blown Lift/Cruise Flap Wind Tunnel Investigation
Author(s): Clark, Rodney L.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-11
Report number: AFFDL TR 73-132
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Examination of the Voice Command Concept for Application to Air Force Cockpits
Author(s): Reising, John M.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-02-05
Report number: AFFDL TR 72-108
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Atmospheric Turbulence Field Parameters Determination
Author(s): Neulieb, Robert L., Golden, Dennis J., Garrison, Jan N.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-04
Report number: AFFDL TR 72-51
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A Study of the Effects of Parameter Variation on the Flying Qualities of the XV-4B V/STOL Aircraft
Author(s): Jones, Arthur G.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-03
Report number: AFFDL TR 72-44
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An Analysis of the Stability and Control Characteristics of an Ejector Wing V/STOL During Transition
Author(s): Kurylowich, George, Martin, James M.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-02
Report number: AFFDL TR 72-37
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The Design of Stability Augmentation Systems for Decoupling Aircraft Responses
Author(s): Pope, Rhall E.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-06
Report number: AFFDL TR 72-63
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An Analytical and Experimental Investigation of Hypersonic Viscous Interaction Pressure Effects
Author(s): Sliski, Neil J.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1973-11
Report number: AFFDL TR 73-58

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