Ignition and combustion characteristics of supersonic combustor under flight Mach number 2.6–3.8
Autor: | Li, Jianping, Wang, Kai, Jiao, Guiqian, Liao, Zilong, Song, Wenyan |
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Zdroj: | In Fuel 1 January 2021 283 |
Databáze: | ScienceDirect |
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