Mean and fluctuating flow measurements in the hypersonic boundary layer over a cooled wall
Measurements of the mean flow, intermittent structure and turbulent fluctuations were made in a cold-wall boundary layer at a stream Mach number of 9·4 and Reynolds number based on momentum thickness of 36 800. For these conditions, the r.m.s. sublayer thickness was 32 times smaller than that of the...
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| Veröffentlicht in: | Journal of fluid mechanics 1974-03, Vol.63 (1), p.121-144 |
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| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Online-Zugang: | Volltext |
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