Experimental research on propulsive performance of the pulse detonation rocket engine with a fluidic nozzle.
| Autor: | Zhang, Qibin1, Wang, Ke1,2 wangk@nwpu.edu.cn, Dong, Rongxiao1, Fan, Wei1,2 weifan419@nwpu.edu.cn, Lu, Wei1, Wang, Yongjia1 |
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| Zdroj: | Energy. Jan2019, Vol. 166, p1267-1275. 9p. |
| Databáze: | Academic Search Ultimate |
| Externí odkaz: |
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