NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A modified wall wake velocity profile for turbulent compressible boundary layers.The law of the wake and the law of the wall in incompressible turbulent boundary layers formulated by Coles (1956) and their use by Mathews et al. (1970) in the development of a wall-wake representation of the velocity profile in a form applicable for isoenergetic compressible boundary layers are extended to a modified wall-wake velocity profile for turbulent compressible boundary layers. The modified wall-wake profile is shown to provide good representations of experimental velocity distributions.
Document ID
19730049637
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Sun, C.-C.
Childs, M. E.
(Washington, University Seattle, Wash., United States)
Date Acquired
August 7, 2013
Publication Date
June 1, 1973
Publication Information
Publication: Journal of Aircraft
Volume: 10
Subject Category
Fluid Mechanics
Accession Number
73A34439
Funding Number(s)
CONTRACT_GRANT: NGR-48-002-047
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available