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首页> 外文期刊>Journal of Spacecraft and Rockets >Investigation of Hypersonic compression Ramp Heating at High Angles of Attack
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Investigation of Hypersonic compression Ramp Heating at High Angles of Attack

机译:高攻角高超声速压缩坡道加热的研究

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摘要

To clarify the relationship of the flow structure and the heating characteristics of blunt-nose flat plates with a compression ramp, an experimental and analytical study of the hypersonic aerodynamic heating characteristics at high angles of attack has been conducted. The effect of nose bluntness and angle of attack on the heating pattern of the compression ramp has been explored, and the relationship between the ramp heating and the shock/shock interaction of the bow, separation, and compression corner shocks were examined.
机译:为了弄清带压缩斜面的钝鼻平板的流动结构和加热特性之间的关系,对高攻角高超声速气动加热特性进行了实验和分析研究。探究了鼻子钝度和迎角对压缩坡道加热方式的影响,并检查了坡道加热与船首的冲击/冲击相互作用,分离和压缩角冲击之间的关系。

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