scramjet combustor

基本解釋

Computations are done on flow configurations that resemble the reaction zone in the scramjet combustor flows.
本文通過數(shù)值模擬得到了超燃沖壓發(fā)動(dòng)機(jī)燃燒室化學(xué)反應(yīng)流流場(chǎng)的流動(dòng)結(jié)構(gòu)。
The results show, in the same entrance condition , the operating mode of scramjet combustor is influenced by the control of fuel .
計(jì)算研究表明，在相同的來流條件下，供油規(guī)律對(duì)燃燒室的工作模態(tài)有著重大的影響；
Scramjet combustor may realize the subsonic-combustion mode and supersonic-combustion mode respectively based on the control of fuel in variable flight conditions.
在不同的來流條件下，可以通過調(diào)節(jié)供油規(guī)律使燃燒室分別實(shí)現(xiàn)亞燃模態(tài)和超燃模態(tài)；