Application of two-dimensional vortex theory to the prediction of flow fields behind wings of wing-body combinations at subsonic and supersonic speeds

Responsibility
Arthur Wm. Rogers.
Imprint
Washington, D.C. : National Advisory Committee for Aeronautics, 1954.
Physical description
[2], 91 p. : ill ; 27 cm.
Series
Technical note (United States. National Advisory Committee for Aeronautics) ; 3227.

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Librarian view | Catkey: 9119349