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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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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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