Arrangement of fusiform bodies to reduce the wave drag at supersonic speeds / Morris D. Friedman and Doris Cohen.

Using linearized slender-body theory and reverse-flow theorems, the wave drag of a system of fusiform bodies at zero angle of attack and supersonic speeds is studied to determine the effect of varying the relative location of the component parts. The investigation is limited to two-body and three-bo...

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Bibliographic Details
Main Author: Friedman, Morris D.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Cohen, Doris
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1954]
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3345.
Subjects:

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Call Number: Y 3.N 21/5:6/3345
Y 3.N 21/5:6/3345 Available Place a Hold