An Energy-bypass system located parallel to combustor has been applied for the performance improvement at high flight speed and extension of flight envelop.
英
美
释义
为了提高冲压发动机在更高速度区内的性能,扩展发动机的运行速度范围,需要在并行于发动机的燃烧室处附加一套能量旁路系统。
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