Combustion characterization of a CH4/O2 rapid mixed swirl torch igniter for hybrid rocket motors
Authors:
- Yi WuYWYi Wu
- Zixiang ZhangZZZixiang Zhang
- Fuwen LiangFLFuwen Liang
- Ningfei WangNWNingfei Wang
- 1 March 2020
- journal article
- research article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 98
Abstract
No abstract availableKeywords
Funding Information
- Youth Science Fund Project
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