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Motion of a gas shock layer with a free boundary under nonadiabatic conditions

โœ Scribed by S. F. Chekmarev


Publisher
Springer
Year
1977
Tongue
English
Weight
174 KB
Volume
11
Category
Article
ISSN
0015-4628

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Study of the shock motion in a hypersoni
โœ C. B. Lee; S. Wang ๐Ÿ“‚ Article ๐Ÿ“… 1995 ๐Ÿ› Springer ๐ŸŒ English โš– 722 KB

Wall pressure fluctuations and surface heat transfer signals have been measured in the hypersonic turbulent boundary layer over a number of compression-corner models. The distributions of the separation shock oscillation frequencies and periods have been calculated using a conditional sampling algor