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: | , , , , , , , |
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| 格式: | Conference item |
| 语言: | English |
| 出版: |
CEAS
2024
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