Two-dimensional compression corner and planar shock wave interactions with a supersonic, turbulent boundary layer /
Theoretical Aerodynamics Research Laboratory (ARL) ; [author, C. Herbert Law].

Description

Main Author

Law, C. Herbert

Related Names

Aerospace Research Laboratories (U.S.)
Aerospace Research Laboratories (U.S.). Theoretical Aerodynamics Research Laboratory.

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Air Force Systems Command, 1975.

Subjects

Turbulent boundary layer.
Shock waves.
Aerodynamic load.
Shock waves.
Turbulent boundary layer.
Aerodynamic load.

Note

"Final report, 1 August 1972-1 February 1975."
"June 1975."
Cover title.

Physical Description

ix, 107 pages : illustrations ; 28 cm

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