タイトル | Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0 |
本文(外部サイト) | http://hdl.handle.net/2060/19650003195 |
著者(英) | Stofan, A. J.; Mihaloew, J. R. |
著者所属(英) | NASA Lewis Research Center |
発行日 | 1961-01-01 |
言語 | eng |
内容記述 | Pumping and internal thrust performance of simulated variable divergent-shroud ejector nozzle designed for flight Mach numbers to 3.0 |
NASA分類 | PROPULSION SYSTEMS |
レポートNO | 65N12796 NASA-TM-X-255 |
権利 | No Copyright |