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Recent developments in rotary-balance testing of fighter aircraft configurations at NASA Ames Research Center 科技报告
报告编号: NASA-TM-86714, REPT-85211, NAS 1.15:86714. 出版年: 1985
作者:  Malcolm, G. N.;  Schiff, L. B.
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AERODYNAMIC BALANCE  AERODYNAMIC CONFIGURATIONS  ANGLE OF ATTACK  F-15 AIRCRAFT  ROTARY STABILITY  STABILITY TESTS  REYNOLDS NUMBER  SPIN  STABILITY DERIVATIVES  WIND TUNNEL TESTS  
A compilation and analysis of helicopter handling qualities data. Volume 1: Data compilation 科技报告
报告编号: NASA-CR-3144, TR-1087-1. 出版年: 1979
作者:  Heffley, R. K.;  Jewell, W. F.;  Lehman, J. M.;  Vanwinkle, R. A.
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BO-105 HELICOPTER  FLIGHT CHARACTERISTICS  H-53 HELICOPTER  HELICOPTER CONTROL  OH-6 HELICOPTER  UH-1 HELICOPTER  AERODYNAMICS  AIRCRAFT DESIGN  DEGREES OF FREEDOM  EQUATIONS OF MOTION  FLIGHT CONDITIONS  STABILITY DERIVATIVES  TRANSFER FUNCTIONS  
A summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow 科技报告
报告编号: NACA-TR-1052. 出版年: 1951
作者:  Jones, Arthur L;  Alksne, Alberta
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AIRCRAFT  AERODYNAMIC STABILITY  AIRCRAFT STABILITY  LATERAL STABILITY  THIN WINGS  SUPERSONIC SPEED  PLANFORMS  COMPRESSIBILITY EFFECTS  STABILITY DERIVATIVES  COMPUTATIONAL FLUID DYNAMICS  TRAPEZOIDAL WINGS  RECTANGULAR WINGS  SWEPTBACK WINGS  DELTA WINGS  DESIGN  CHARTS