タイトル | Investigation of a nearly isentropic mixed compression axisymmetric inlet system at Mach numbers 0.6 to 3.2 |
本文(外部サイト) | http://hdl.handle.net/2060/19680013885 |
著者(英) | Sorensen, N. E.; Smeltzer, D. B. |
著者所属(英) | NASA Ames Research Center |
発行日 | 1968-05-01 |
言語 | eng |
内容記述 | Wind tunnel tests of mixed-compression axisymmetric inlet system to determine bleed mass flow ratio, pressure recovery and pressure distortion |
NASA分類 | PROPULSION SYSTEMS |
レポートNO | 68N23354 NASA-TN-D-4557 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/212013 |