Abstract
A summary is given of the recent experimental data on the structure of turbulent boundary layers in supersonic flow. The physical mechanisms differentiating incompressible and compressible boundary layers are discussed. A simple model for the Mach and Reynolds number dependence of the decay of the large-scale motions is proposed.
| Original language | English (US) |
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| State | Published - Dec 1 1990 |
| Event | Twelfth Turbulence Symposium - Rolla, MS, USA Duration: Sep 24 1990 → Sep 26 1990 |
Other
| Other | Twelfth Turbulence Symposium |
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| City | Rolla, MS, USA |
| Period | 9/24/90 → 9/26/90 |
All Science Journal Classification (ASJC) codes
- Engineering(all)