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An Analytical Study Of The Dynamics Of Spinning Aircraft. Part 2. Wind Tunnel Tests
Author(s): Wykes, John H., Casteel, Gilbert R., Collins, Richard A.Corporate Author(s): North American Aviation, Inc.
Laboratory: Flight Control Laboratory
Date of Publication: 1958-12
Report number: WADC TR 58-381 Part 2
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The Operation Of Manned Spacecraft
Author(s): Bamford, Harold E., Hanes, Lewis F. , Ritchie, Malcolm L., Wilson, Summitt E.Corporate Author(s): Ritchie And Associates, Inc; Lear, Inc
Laboratory: Flight Control Laboratory
Date of Publication: 1958-06
Report number: WADC TR 58-225
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Summary Of Component Failure Rate And weighting Function Data And Their Use In Systems Preliminary Design
Author(s): Johnston, Donald E., McRuer, Duane T.Corporate Author(s): Control Specialists Division, Kelsey-Hayes
Laboratory: Flight Control Laboratory
Date of Publication: 1957-12
Report number: WADC TR 57-668
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A Study of the Nature of Atmospgeric Trubulence Based Upon Flight Measurement of the Gust Velocity Components
Author(s): None GivenCorporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Flight Control Laboratory
Date of Publication: 1957-05
Report number: WADC TR 57-259
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Boundary Layer Control Applied To Tail Surfaces Of A Aircraft . Part II: Final Report
Author(s): Gersten, W. M., Wise, W. D.Corporate Author(s): Cessna Aircraft Company
Laboratory: Flight Control Laboratory
Date of Publication: 1957-12
Report number: WADC TR 57-741 Part 2
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Boundary Layer Control Applied To Tail Surfaces Of Aircraft . Part I: Wind Tunnel Report
Author(s): Leisher, L. L., Gertsen, W. M.Corporate Author(s): Cessna Aircraft Company
Laboratory: Flight Control Laboratory
Date of Publication: 1957-12
Report number: WADC TR 57-741 Part 1
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Study To Determine An Automatic Flight Control Configuration To Provide A Stability Augmentation Capability For High Performance Supersonic Aircraft
Author(s): Van Meter, J. T., McLane, R. C.Corporate Author(s): Minneapolis-Honeywell Regulator Company
Laboratory: Flight Control Laboratory
Date of Publication: 1957-06
Report number: WADC TR 57-349
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A Study Of Angle-of-attack Angle-of-sideslip Pitot-static Probes
Author(s): Smetana, Frederick O., Stuart, Jay Wm., Jr.Corporate Author(s): University of Southern California
Laboratory: Flight Control Laboratory
Date of Publication: 1958-01
Report number: WADC TR 57-234
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Human Pilot Dynamic Response In Flight And Simulator
Author(s): Seckel, Edward, Hall, Ian A. M.Corporate Author(s): James Forrestal Research Center, Princeton University
Laboratory: Flight Control Laboratory
Date of Publication: 1958-08
Report number: WADC TR 57-520
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Research and Development of a Hot Gas Flight Stabilization System
Author(s): Eclipse- Pioneer Div., Bendix Aviation Corp.Corporate Author(s): Eclipse-pioneer Div. Bendix Aviation Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1960-09
Report number: WADD TR 60-449 Part I Volume I
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