Abstract
Theoretical estimates and computational analysis of the role of temperature gradients, non-uniform heating, and wall effects in determining structure of propagating shocks in glow discharges and of bow shocks around moving spheres is performed. The multi-peak structure of density-gradient shock profiles observed in glow discharges is shown to be consistent with gas dynamic effects of shock distortion and complex flow structure caused by transverse temperature gradients. A possible role of finite geometry combined with non-uniform temperature distribution in ballistic range studies is analyzed. Vibrational relaxation phenomena are indicated as potentially important in determining bow shock structure around blunt bodies moving through molecular plasmas.
| Original language | English (US) |
|---|---|
| State | Published - 1999 |
| Event | 37th Aerospace Sciences Meeting and Exhibit, 1999 - Reno, United States Duration: Jan 11 1999 → Jan 14 1999 |
Other
| Other | 37th Aerospace Sciences Meeting and Exhibit, 1999 |
|---|---|
| Country/Territory | United States |
| City | Reno |
| Period | 1/11/99 → 1/14/99 |
All Science Journal Classification (ASJC) codes
- Space and Planetary Science
- Aerospace Engineering