| タイトル | Variable stream control engine concept for advanced supersonic aircraft: Features and benefits |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770011068 |
| 著者（英） | Howlett, R. A. |
| 著者所属（英） | Pratt and Whitney Aircraft Group |
| 発行日 | 1976-01-01 |
| 言語 | eng |
| 内容記述 | The Variable Stream Control Engine is studied for advanced supersonic cruise aircraft. Significant environmental and performance improvements relative to first generation supersonic turbojet engines are cited. Two separate flow streams, each with independent burner and nozzle systems are incorporated within the engine. By unique control of the exhaust temperatures and velocities in two coannular streams, significant reduction in jet noise is obtained. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 77N18012 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/569719 |
