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Mixing length in low Reynolds number compressible turbulent boundary layersThe paper studies the effect of low Reynolds number in high-speed turbulent boundary layers on variations of mixing length. Boundary layers downstream of natural transition on plates, cones and cylinders, and boundary layers on nozzle walls without laminarization-retransition are considered. The problem of whether low Reynolds number amplification of shear stress is a result of transitional flow structure is considered. It is concluded that a knowledge of low Reynolds number boundary layer transition may be relevant to the design of high-speed vehicles.
Document ID
19760031027
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bushnell, D. M.
(NASA Langley Research Center Hampton, VA, United States)
Cary, A. M., Jr.
(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: AIAA Journal
Volume: 13
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
76A13993
Distribution Limits
Public
Copyright
Other

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