| タイトル | Enhanced capability of the Combustion-Heated Scramjet Test Facility |
| 著者（英） | Andrews, Earl H.; Eggers, James M.; Rock, Kenneth E. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1991-06-01 |
| 言語 | eng |
| 内容記述 | The Combustion-Heated Scramjet Test Facility (CHSTF) is described together with its modifications. The expanded simulation capabilities of the facility are documented. Nozzle exit surveys and tunnel calibration information are presented. It is noted that these modifications included a new heat-sink nickel liner heater, a new Mach 4.7 nozzle, and a new 70-ft vacuum sphere exhaust system. It is found that the facility in the air ejector mode of operation performed similarly to that prior to the addition of the vacuum sphere ducting. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 91A44267
AIAA PAPER 91-2502 |
| 権利 | Copyright |
