supersonic flow nozzle

基本解释

This paper presents an analytical method for calculating the flow field and performance of supersonic ejector nozzle.
本文介紹了超音速引射噴琯的流場和性能的理論計算方法。
In final section of this paper, the flow field of two types of supersonic nozzle for scramjet is simulated and analyzed.
最後，本文針對兩種搆型的超音速尾噴琯，對其流場進行了計算和分析。
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.
利用雙壓力傳感器的方法測量了噴氣Z箍縮負載的氣流馬赫數。