A Turbulent Model Study for the Multicomponent Nonsimilar Turbulent Boundary Layer Program
Technical rept. May 1970-Mar 1971
AEROTHERM CORP MOUNTAIN VIEW CA
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An investigation of the accuracy of the Air Force Weapons Laboratory Nonsimilar Turbulent Boundary Layer Computer Code through comparisons of predictions with experimental data is presented. Five complete data sets are selected from a literature survey of flat plate supersonic flow, hypersonic flow with and without accerleration, supersonic flow with highly nonsimilar wall temperature wall blowing. Comparisons are presented which include velocity, total temperature, and Mach number profiles at several axial stations.
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