An assessment is given of existing shock wave/tubulent boundary-layer interaction experiments having sufficient quality to guide turbulence modeling and code validation efforts. Although the focus of this work is hypersonic, experiments at Mach numbers as low as 3 were considered. The principal means of identifying candidate studies was a computerized search of the AIAA Aerospace Database. Several hundred candidate studies were examined and over 100 of these were subjected to a rigorous set of acceptance criteria for inclusion in the data-base. Nineteen experiments were found to meet these criteria, of which only seven were in the hypersonic regime (M is greater than 5).
Supersonic and hypersonic shock/boundary-layer interaction database
AIAA Journal ; 32 , 7
1994-07-01
Miscellaneous
No indication
English
Supersonic and Hypersonic Shock-Boundary-Layer Interaction Database
Online Contents | 1994
|Hypersonic shock/boundary-layer interaction database
AIAA | 1991
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