Abstract

The results of the calculation of the interaction of a supersonic jet flowing at a zero angle of attack from the frontal surface of the body of rotation to the opposite supersonic flow at different supersonic Mach numbers of the flow and jet are given. The influence of the total pressure in the gas flow and in the jet on the structure of the emerging gas flow is considered.

中文翻译：

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旋转体正面射流与逆流相互作用中的流动结构计算

摘要

给出了不同超音速马赫数下从旋转体正面以零攻角流动的超音速射流与相反的超音速流相互作用的计算结果。考虑了气流和射流中的总压力对出现的气流的结构的影响。