Experimental performance evaluation of a streamline traced inlet at off-design conditions
Scramjet engines used as part of a multi-stage space access system must operate efficiently over a wide range of conditions. This paper describes experimental testing undertaken to evaluate the masscapture performance, self-starting capability, and back-pressure limitations of a streamline-traced th...
| Main Authors: | , , , , , , , |
|---|---|
| 格式: | Conference item |
| 語言: | English |
| 出版: |
CEAS
2024
|