Minimum-drag ducted and pointed bodies of revolution based on linearized supersonic theory / Hermon M. Parker.

The linearized drag integral for bodies of revolution at supersonic speeds is presented in a double-integral form which is not based on slender-body approximations but which reduces to the usual slender-body expression in the proper limit. With the aid of a suitably chosen auxiliary condition, the m...

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Bibliographic Details
Main Author: Parker, Hermon M.
Corporate Author: United States. National Advisory Committee for Aeronautics
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) ; 3189.
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Call Number: Y 3.N 21/5:6/3189
Y 3.N 21/5:6/3189 Available Place a Hold