Turbulence two phase flow and combustion process in a liquid rocket engine combustor are analyzed with numerical method, and combustion instability is also studied.
采用数值模拟的方法对液体火箭发动机燃烧室内湍流两相流动与燃烧过程进行了分析，同时研究了燃烧室内高频不稳定燃烧现象。
This engine consists of an inlet, a combustor, and a nozzle .
这台发动机由一个进气道，一个燃烧室和一个尾喷管组成。
The operating principle of a ramgen is introduced, and a new concept of tangential trapped vortex combustor (TTVC) used for the engine is presented.
介绍了冲压转子发动机的工作原理，提出了适用于这种发动机的切向驻涡燃烧室新概念；
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