タイトル | Investigation of a large-scale mixed compression axisymmetric inlet system capable of high performance at Mach numbers 0.6 to 3.0 |
本文(外部サイト) | http://hdl.handle.net/2060/19680007559 |
著者(英) | Sorensen, N. E.; Smeltzer, D. B. |
著者所属(英) | NASA Ames Research Center |
発行日 | 1968-02-01 |
言語 | eng |
内容記述 | Design and performance testing of large scale mixed compression axisymmetric inlet at transonic and supersonic speeds |
NASA分類 | PROPULSION SYSTEMS |
レポートNO | 68N17028 NASA-TM-X-1507 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/212445 |