Abstract
The effects of varying Mach and Reynolds numbers on the behavior of turbulent boundary layers is discussed. The emphasis is on the evaluating the relevance of subsonic experience to the interpretation of supersonic flows.
| Original language | English (US) |
|---|---|
| DOIs | |
| State | Published - 1995 |
| Event | 33rd Aerospace Sciences Meeting and Exhibit, 1995 - Reno, United States Duration: Jan 9 1995 → Jan 12 1995 |
Other
| Other | 33rd Aerospace Sciences Meeting and Exhibit, 1995 |
|---|---|
| Country/Territory | United States |
| City | Reno |
| Period | 1/9/95 → 1/12/95 |
All Science Journal Classification (ASJC) codes
- Space and Planetary Science
- Aerospace Engineering