Scramjet nozzle was installed at the exit of the combustor.

尾喷管直接安装在模型发动机的燃烧室出口.

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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.

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This paper summarized the latestand foreign development status of scramjet engine andthe key technologies.

超燃冲压发动机技术是一项新型的、具有广阔发展前景的推进技术.

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