The airframe and engine highly integration nature of hypersonic vehicle results in the asymmetry and cowl adjustable characters of the scramjet nozzle.
由于高超声速飞行器机体与发动机高度一体化的构型,使超燃冲压发动机尾喷管具有非对称,面罩可调等特点。
参考来源 - 超燃冲压发动机尾喷管仿真和试验研究·2,447,543篇论文数据，部分数据来源于NoteExpress
提出了超燃冲压发动机燃烧室的性能分析评价方法。
The methodology for scramjet combustor performance analysis and evaluation is build up.
再生冷却技术是超燃冲压发动机燃烧室热防护的关键技术。
Regenerative cooling technology is one of the key technologies to thermally protect scramjet chamber.
不过，太空署要如何使得超燃冲压发动机进入持续飞行需要的超音速呢？
But how does NASA plan to get the scramjet to the supersonic speeds necessary for sustained flight?
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