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Calculation of a separated turbulent boundary layerThe properties of a Navier-Stokes solution of a shock-separated turbulent flow over a flat wall are investigated. Refinements of an algebraic relaxation turbulence model previously shown to be of value for the simulation of separated flows are presented. A simplified analysis applicable near an adiabatic wall is developed and used to help verify the accuracy of the numerical solution. Features of the time-dependent response of a turbulent boundary layer to shock impingement are presented.
Document ID
19770003419
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baldwin, B.
(NASA Ames Research Center Moffett Field, CA, United States)
Hung, C. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Advan. in Eng. Sci., Vol. 4
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
77N10361
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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