| タイトル | Computations of non-reacting and reacting viscous blunt body flows, volume 2 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730011583 |
| 著者（英） | Li, C. P. |
| 著者所属（英） | Lockheed Electronics Co. |
| 発行日 | 1973-02-01 |
| 言語 | eng |
| 内容記述 | Computer programs for calculating the flow distribution in the nose region of a blunt body at arbitrary speed and altitude are discussed. The programs differ from each other in their ability to consider either thin shock or thick shock conditions and in the use of either ideal, equilibrium air, or nonequilibrium air chemistry. The application of the programs to analyzing the flow distribution around the nose of the shuttle orbiter during reentry is reported. |
| NASA分類 | FLUID MECHANICS |
| レポートNO | 73N20310
TR2007-VOL-2
NASA-CR-128872 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/199958 |
