| タイトル | Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream Mach number of zero |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840005093 |
| 著者（英） | Putnam, L. E.; Strong, E. G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1983-12-01 |
| 言語 | eng |
| 内容記述 | An investigation was conducted in the static test facility of the Langley 16-Foot Transonic Tunnel to measure static pressure distributions inside a nonaxisymmetric thrust reversing nozzle. The tests were made at nozzle total pressures ranging from ambient to about eight times ambient pressure at a free stream Mach number of zero. Tabulated pressure data are presented. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 84N13161
NAS 1.15:85655
L-15582
NASA-TM-85655 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/160973 |
