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. Jones, Robert M. Sorenson, and Elizabeth E. Lindler.

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 potent...

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Main Author: Jones, A. L. (Arthur Leslie)
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Sorenson, Robert M., Lindler, Elizabeth E.
Other title:Technical report archive and image library.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1949.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 1916.
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Call Number: Y 3.N 21/5:6/1916
Y 3.N 21/5:6/1916 Available Place a Hold