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Computing incompressible laminar and turbulent boundary layer formationProgram generates initial laminar conditions, such as in Falkner-Skan similarity flows, or turbulent equilibrium profiles. Initial profile input data is used. Combination with inviscid-freestream calculations to predict entire flow field in turbine cascade or around airfoil is possible.
Document ID
19710000154
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Herring, H. J. (PRINCETON UNIV.)
Mellor, G. L.
Date Acquired
August 6, 2013
Publication Date
May 1, 1971
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LEW-11190
Report Number: LEW-11190
Accession Number
71B10155
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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