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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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- Paiewonsky, Bernard H. (2)
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- Flight Control Laboratory (5)
- Yale University (3)
- Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology (1)
- Aeronautical Equipment Division, Sperry Gyroscope Company (1)
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