Scramjet nozzle was installed at the exit of the combustor.
尾噴管直接安裝在模型發(fā)動機的燃燒室出口.
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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)動機燃燒室化學反應(yīng)流流場的流動結(jié)構(gòu).
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This paper summarized the latestand foreign development status of scramjet engine andthe key technologies.
超燃沖壓發(fā)動機技術(shù)是一項新型的、具有廣闊發(fā)展前景的推進技術(shù).
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