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An invariant second-order closure model of the compressible turbulent boundary layer on a flat plateThe development of an invariant model designed expressly for the computation of shear flows is discussed. The model for incompressible layers seeks a second-order closure of the equations for the mean and fluctuating fields. The development of a method for computing the behavior of shear layers in compressible forces is described. The complexity of the analysis is restrained by limiting the consideration to a flat plate boundary layer where the mean pressure can be taken to be constant.
Document ID
19720024343
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Donaldson, C. D. (Aeronautical Research Associates of Princeton, Inc. Princeton, NJ, United States)
Sullivan, R. D. (Aeronautical Research Associates of Princeton, Inc. Princeton, NJ, United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-128172
Accession Number
72N31993
Funding Number(s)
CONTRACT_GRANT: NASW-2224
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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