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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