The linearized subsonic flow about symmetrical nonlifting wing-body combinations / John B. McDevitt.

Methods are presented for determining the linearized subsonic flow about symmetrical, nonlifting wing-body combinations. The wing is represented by a suitable planar distribution of elementary sources in accordance with the usual assumptions of linearized, thin-airfoil theory. The required boundary...

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Bibliographic Details
Main Author: McDevitt, John B.
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington : National Advisory Committee for Aeronautics, [1957]
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3964.
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Call Number: Y 3.N 21/5:6/3964
Y 3.N 21/5:6/3964 Available Place a Hold