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The Effects of Sideslip, Aspect Ratio, and Mach Number on the Lift and Pitching Moment of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

Arthur L. JonesRobert M. SorensonElizabeth E. Lindler

出版	National Advisory Committee for Aeronautics, 1949
URL	http://books.google.com.hk/books?id=ZAFBecgHudsC&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋The variations of lift and pitching moment with sideslip in supersonic flow have been calculated for a representative gorup of plan forms. The variations of lift and pitching moment with aspect ratio and Mach number at zero sideslip were also investigated. The analysis was based on linearized potential theory and was applied to triangular, trapezoidal, rectangular, and swept-back plan forms without dihedral.