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19 items
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Spin and Recovery Tests of a 1/28-Scale Model of the YF-93A Airplane
Author(s): Rose, Eugene S., Jr., Parker, Dan M.Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1952-08
Report number: WADC TR 52-206
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Rigid Tow Bar for C-82 Type Aircraft
Author(s): Jones, Arthur G.Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1952-08
Report number: WADC TR 52-167
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A Development of the Longitudinal Dynamic Equations of Motion of an Aircraft at the Absolute Ceiling
Author(s): Robinson, Alfred C., Doody, Bernard J.Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1955-05
Report number: WADC TR 55-210
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The Air Force Program For Improved Flight Instrumentation
Author(s): Wright, Lawrence C.Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-11
Report number: WADC TR 56-582
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Simulation Study Of Control Of An Aircraft At Or Near The Absolute Ceiling
Author(s): Robinson, Alfred C., Early, James W., Doody, Bernard J.Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-03
Report number: WADC TR 56-39
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The Effects Of Engine Angular Momentum On An Airplane's Longitudinal And Lateral-Directional Dynamic Stability
Author(s): Paiewonsky, Bernard H.Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-06
Report number: WADC TR 56-225
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The Influence Of Geometry Parameters Upon Lag Error In Airborne Pressure Measuring Systems
Author(s): Lamb, J. P., Jr.Corporate Author(s): Flight Control Laboratory
Date of Publication: 1957-07
Report number: WADC TR 57-351
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A Method for Estimating Damping Derivatives of VTOL Aircraft in Transition and Hovering Flight
Author(s): Paiewonsky, Bernard H.Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-09
Report number: WADC TN 56-410
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Investigation of a Technique for Improving Aircraft Response Using a Complementary Optimum-Response Model
Author(s): Rath, Raymond R.Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-09
Report number: WADC TN 56-475
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The Air Force Integrated Flight Instrument Panel
Author(s): Svimonoff, ConstantineCorporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1958-10
Report number: WADC TR 58-431
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- Doody, Bernard J. (2)
- Gregory, P. C. (2)
- Paiewonsky, Bernard H. (2)
- Robinson, Alfred C. (2)
- Schwartz, Lawrence (2)
- Early, James W. (1)
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