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Mach and Reynolds number effects on turbulent skin friction reduction by injectionThe investigation reported is concerned with questions regarding a possible Mach number influence on skin friction reduction caused by injection. The investigation shows that data considered by Danberg (1967) for the no-blowing skin friction coefficient are in error. Accurate profiles and local skin friction coefficient values are obtained when the influence of low Reynolds number amplification in the outer region of the boundary layer is included in a calculation method.
Document ID
19760031331
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bushnell, D. M. (NASA Langley Research Center Hampton, VA, United States)
Watson, R. D. (NASA Langley Research Center Hampton, VA, United States)
Holley, B. B. (NASA Langley Research Center High-Speed Aerodynamics Div., Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 12
Subject Category
Aerodynamics
Accession Number
76A14297
Distribution Limits
Public
Copyright
Other

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