Title: Three-dimensional hypersonic transitional/turbulent mean flow profiles
Abstract: Detailed three-dimensional compressible transitional/turbulent boundary-layer profiles are presented for use as test cases in numerical and integral calculation procedures. The profiles were obtained from tests conducted in the Mach 20 leg of the Langley High Reynolds Number Helium Facility. The presented data represent an arduous test case for analytical prediction methods, since 'low Reynolds number' and precursor transition effects should probably be accounted for to accurately predict the boundary-layer growth and development.
Publication Year: 1973
Publication Date: 1973-07-16
Language: en
Type: article
Indexed In: ['crossref']
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