Theoretical pressure distributions on wings of finite span at zero incidence for mach numbers near 1 /
by Alberta Y. Alksne and John R. Spreiter.

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Main Author: Alksne, Alberta Y.
Related Names: Spreiter, John R.
United States. National Aeronautics and Space Administration.
Ames Research Center.
Language(s): English
Published: Washington, D.C. : U.S. G.P.O., 1961.
Subjects: Airplanes > Airplanes / Wings.
Aerodynamics, Transonic.
Physical Description: 47 p. : fig., tabl. ; 26 cm.
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