Dong et al., 2020 - Google Patents
Numerical investigation on flow and mixing characteristics inside a converging-diverging mixing duct of rocket-based combined-cycle engine in ejector modeDong et al., 2020
- Document ID
- 15334107856586385345
- Author
- Dong Z
- Sun M
- Wang Z
- Cai Z
- Yao Y
- Gu R
- Publication year
- Publication venue
- Aerospace Science and Technology
External Links
Snippet
The supersonic mixing layers with complex background waves are formed by the rocket jet and the entrained air in the mixing section of rocket-based combined-cycle (RBCC) engine during ejector mode. To achieve mixing enhancement of primary and secondary flows in …
- 238000009114 investigational therapy 0 title description 15
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