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A Simple Relationship Between the Shock and Expansion Pressure Coefficients as a Basis for Studying Two-Dimensional Hypersonic Flow

机译:冲击和膨胀压力系数的简单关系作为研究二维高超声速流动的基础

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摘要

A simple relation between the two-dimensional wedge pressure coefficients for shock and expansion is shown to apply for the entire hypersonic regime. As a consequence, the hypersonic small-disturbance theory expressions for these coefficients are further simplified as are calculations of pressure distributions on arbitrary two-dimensional configurations at hypersonic speeds. (Author)

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