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

APA Citation

Alksne, A. Y., Spreiter, J. R., United States. National Aeronautics and Space Administration., Ames Research Center. (1961). Theoretical pressure distributions on wings of finite span at zero incidence for mach numbers near 1. Washington, D.C.: U.S. G.P.O..

MLA Citation

Alksne, Alberta Y, John R Spreiter, United States. National Aeronautics and Space Administration, and Ames Research Center. Theoretical Pressure Distributions On Wings of Finite Span At Zero Incidence for Mach Numbers Near 1. Washington, D.C.: U.S. G.P.O., 1961.