scramjet combustor

基本解释

Computations are done on flow configurations that resemble the reaction zone in the scramjet combustor flows.
本文通过数值模拟得到了超燃冲压发动机燃烧室化学反应流流场的流动结构。
The results show, in the same entrance condition , the operating mode of scramjet combustor is influenced by the control of fuel .
计算研究表明，在相同的来流条件下，供油规律对燃烧室的工作模态有着重大的影响；
Scramjet combustor may realize the subsonic-combustion mode and supersonic-combustion mode respectively based on the control of fuel in variable flight conditions.
在不同的来流条件下，可以通过调节供油规律使燃烧室分别实现亚燃模态和超燃模态；