supersonic flow nozzle

基本解释

This paper presents an analytical method for calculating the flow field and performance of supersonic ejector nozzle.
本文介绍了超音速引射喷管的流场和性能的理论计算方法。
In final section of this paper, the flow field of two types of supersonic nozzle for scramjet is simulated and analyzed.
最后，本文针对两种构型的超音速尾喷管，对其流场进行了计算和分析。
The Mach number of the gas flow from the supersonic nozzle in a gas puff Z pinch was determined by the two pressure transducer method.
利用双压力传感器的方法测量了喷气Z箍缩负载的气流马赫数。