Scramjet nozzle was installed at the exit of the combustor.
尾噴管直接安裝在模型發動機的燃燒室出口.
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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構.
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This paper summarized the latestand foreign development status of scramjet engine andthe key technologies.
超燃沖壓發動機技術是一項新型的、具有廣闊發展前景的推進技術.
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