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The similarity law for hypersonic flow and requirements for dynamic similarity of related bodies in free flight

机译:高超声速流动的相似律及自由飞行中相关体动力相似性的要求

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The similarity law for nonsteady, inviscid, hypersonic flow about slender three-dimensional shapes is derived. Conclusions drawn are shown to be valid for rotational flow. Requirements for dynamic similarity of related shapes in free flight are obtained. The law is examined for steady flow about related three-dimensional shapes. Results of an experimental investigation of the pressures acting on two inclined cones are found to check the law as it applies to bodies of revolution.

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