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Slip velocity method for three-dimensional compressible turbulent boundary layersA slip velocity method for 2-D incompressible turbulent boundary layers was presented in AIAA Paper 88-0137. The inner part of the boundary layer was characterized by a law of the wall and a law of the wake, and the outer part was characterized by an arbitrary eddy viscosity model. In the present study for compressible flows, only a law of the wall is considered. The problem of 2-D compressible flow is treated first; then the extension to 3-D flow is addressed. A formulation for primitive variables is presented.
Document ID
19880011208
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Barnwell, Richard W.
(NASA Langley Research Center Hampton, VA, United States)
Wahls, Richard A.
(North Carolina State Univ. Raleigh., United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1988
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-100586
NAS 1.15:100586
Report Number: NASA-TM-100586
Report Number: NAS 1.15:100586
Accession Number
88N20592
Funding Number(s)
PROJECT: RTOP 763-01-21-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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