experimental study on rbcc with oxygen/kerosene firstly combustion
- Paper number
IAC-13,C4,9,5,x16945
- Author
Dr. Liang Tian, Beihang University, China
- Year
2013
- Abstract
Oxygen/kerosene were used as the firstly combustion propellants to text RBCC on Direct-connected. Rocket ejector with strut characteristic was adopted, and composite injection with strut and wall was used to the secondly combustion. Mass follow rate of rocket ejector, number of nozzle and injection methods were investigated. The results show that, the added fuel can be ignited by fuel-rich gas which was generated by oxygen/kerosene combustion; reasonable composite injection can enhance RBCC performance.
- Abstract document
- Manuscript document
IAC-13,C4,9,5,x16945.pdf (🔒 authorized access only).
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