A numerical investigation of injection angle effect on lateral jet interaction for revolution body

【Author】

Yuwei Liu;Zhaoyong Ni;Yaofeng Liu;

【Abstract】

<正>A numerical investigation has been conducted to determine injection angle effect on lateral jet interaction for a revolution body in hypersonic flow.Air is injected through a nozzle at 30°to 150°into a Mach 5.0 crossflow.Surface and space flow features of

【Keywords】

A numerical investigation of injection angle effect on lateral jet interaction for revolution body;

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