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Exploratory investigations of the effects of gas injection through a porous model on separation, transition, static stability and control effectiveness of a blunt entry body at Mach number 7.3

机译:通过多孔模型注入气体对马赫数为7.3的钝入口体的分离,过渡,静态稳定性和控制效果的探索性研究

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Hypersonic wind tunnel tests of gaseous injection effects from wall of blunt reentry body model on separation, transition, static stability, and control effectiveness

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