| タイトル | Exit of a blast wave from a conical nozzle |
| 著者（英） | Johnson, W. E.; Kim, K. |
| 著者所属（英） | Lockheed Aircraft Service Co. |
| 発行日 | 1976-07-01 |
| 言語 | eng |
| 内容記述 | The Eulerian computer code DORF was used in the analysis of a two-dimensional, unsteady flow field resulting from semi-confined explosions for propulsive applications. Initially, the ambient gas inside the conical shaped nozzle is set into motion due to the expansion of the explosion product gas, forming a shock wave. When this shock front exits the nozzle, it takes almost a spherical form while a complex interaction between the nozzle and compression and rarefaction waves takes place behind the shock. The results show an excellent agreement with experimental data. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 76A39869
AIAA PAPER 76-401 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/442376 |
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