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 this paper, the flow field of the supersonic diffuser and the subsonic-supersonic ejector is simulated by numerical method.
本文采用上述数值算法模拟了超声速扩压器和超声速引射器内流场。
The calculated results agree well with the test results and it shows that the numerical methods can be used for the study of the supersonic ejector.
计算结果与实验结果符合较好，这表明该数值方法是研究超声速引射器的一种重要研究手段。
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