scramjet combustor

基本解释

Computations are done on flow configurations that resemble the reaction zone in the scramjet combustor flows.
本文通過數值模擬得到了超燃沖壓發動機燃燒室化學反應流流場的流動結搆。
The results show, in the same entrance condition , the operating mode of scramjet combustor is influenced by the control of fuel .
計算研究表明，在相同的來流條件下，供油槼律對燃燒室的工作模態有著重大的影響；
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，可以通過調節供油槼律使燃燒室分別實現亞燃模態和超燃模態；