| タイトル | Operating characteristics of the Langley Mach 7 Scramjet Test Facility |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810011555 |
| 著者（英） | Sabol, A. P.; Torrence, M. G.; Guy, R. W.; Mueller, J. N. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1981-03-01 |
| 言語 | eng |
| 内容記述 | Operating characteristics of the Langley Mach 7 Scramjet Test Facility are described. The facility is designed for testing airframe integrated scramjet (supersonic combustion ramjet) engine models. Features include duplication of the flight Mach number total enthalpy, flight altitude simulation, and simulation of engine airframe integration effects such a bow shock wave precompression and boundary layer ingestion by the engine. Data obtained from facility calibration and from tests of a hydrogen burning, airframe integrated scramjet are discussed. An adverse interaction between the facility flow and the scramjet engine flow during combustion of the fuel is described. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 81N20083
L-14174
NASA-TM-81929 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/169745 |
