| タイトル | Pitot-Pressure Measurements in Flow Fields Behind a Rectangular Nozzle with Exhaust Jet for Free-Stream Mach Numbers of 0.00, 0.60, and 1.20 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19870002263 |
| 著者（英） | Putnam, L. E.; Mercer, C. E. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1986-11-01 |
| 言語 | eng |
| 内容記述 | An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to measure the flow field in and around the jet exhaust from a nonaxisymmetric nozzle configuration. The nozzle had a rectangular exit with a width-to-height ratio of 2.38. Pitot-pressure measurements were made at five longitudinal locations downstream of the nozzle exit. The maximum distance downstream of the exit was about 5 nozzle heights. These measurements were made at free-stream Mach numbers of 0.00, 0.60, and 1.20 with the nozzle operating at a ratio of nozzle total pressure to free-stream static pressure of 4.0. The jet exhaust was simulated with high-pressure air that had an exit total temperature essentially equal to the free-stream total temperature. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 87N11696
L-16166
NAS 1.15:88990
NASA-TM-88990 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/82187 |
