Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 8 /
P. Calvin Stainback.

Description

Main Author

Stainback, P. Calvin.

Related Names

Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1969.

Subjects

Aerodynamics, Hypersonic.
Angle of attack (Aerodynamics)
Noses (Space vehicles)
Reynolds number.

Physical Description

76 p. : ill. ; 27 cm.

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