Reynolds number effects on the induced pressures of cylindrical bodies with different nose shapes and nose drag coefficients in helium at a Mach number of 24 /
Richard D. Wagner, Jr., and Ralph Watson.

Description

Main Author: Wagner, Richard D., Jr.
Related Names: Watson, Ralph.
Langley Research Center.
United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1963.
Subjects: Mach number.
Reynolds number.
Aerodynamics.
Physical Description: 40 p. : ill. ; 27 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign