| タイトル | An experimental investigation of a highly underexpanded sonic jet ejecting from a flat plate into a subsonic crossflow |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740003703 |
| 著者（英） | Margason, R. J.; Shaw, C. S. |
| 著者所属（英） | Army Air Mobility Research and Development Lab.|NASA Langley Research Center |
| 発行日 | 1973-12-01 |
| 言語 | eng |
| 内容記述 | The induced static pressures due to a highly underexpanded sonic jet ejecting normally from a flat plate into a subsonic crosswind have been investigated. These pressure data have been recorded on the flat plate for a range of nominal jet-to-free-stream dynamic-pressure ratios from 0 to 1000 at free-stream Mach numbers of 0.1, 0.2, 0.4, and 0.6. The static pressure data measured on the flat plate are presented and correlated based upon the Riemann shock geometry in the jet plume. This data correlation improves with increasing free-stream Mach number. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 74N11816
NASA-TN-D-7314
L-8863 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/196767 |
