| タイトル | Thrust and pumping characteristics of cylindrical ejectors using afterburning turbojet gas generator |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730023889 |
| 著者（英） | Huntley, S. C.; Samanich, N. E. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1969-01-01 |
| 言語 | eng |
| 内容記述 | Static tests of cylindrical ejectors having ejector to primary diameter ratios from 1.1 to 1.6 and ejector length to primary nozzle diameter ratios from 0.9 to 2.1 are reported. Power setting of the J85-13 turbojet engine was varied from part power to maximum afterburning. Corrected secondary weight flow ratio was varied from 0.02 to 0.08 over a range of exhaust nozzle pressure ratios from 2.0 to 9.0. Secondary flow temperature rise and pressure drop characteristics through the nacelle secondary flow passage were also obtained. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 73N32622
NASA-TM-X-52565 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/197406 |
