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Comments on Crocco's solution and the independence principle for compressible turbulent boundary layersThe purpose of the present note is to show that on a flat plate where both the wall temperature and mean wall pressure are constant, neither of the limitations of parallel flow or of unity for the turbulent Prandtl number are required in order for the Crocco solution to apply to the turbulent boundary-layer flow. It is shown herein that this result is subject to restrictions on the magnitude of pressure fluctuations. The same analysis is generalized to show that the compressible turbulent boundary layer on an isothermal swept flat plate is independent of the spanwise flow if the molecular Prandtl number is unity.
Document ID
19740037544
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Beckwith, I. E.
(NASA Langley Research Center Hypersonic Vehicles Div., Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
February 1, 1974
Publication Information
Publication: AIAA Journal
Volume: 12
Subject Category
Fluid Mechanics
Accession Number
74A20294
Distribution Limits
Public
Copyright
Other

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