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On Shock Polar Solutions of Pseudo-Steady Mach Reflections

机译:关于伪稳态马赫反射的激极解

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摘要

This paper investigates the three-shock theoretical shock polar solutions of pseudo-steady MR as functions of initial conditions of M_s (incident shock Mach number) and θ_w (reflecting wedge angle) for γ= 1.4. Different possible shock polar solutions of pseudo-steady MR from the three-shock theory satisfying the normal straight Mach stem boundary condition are discussed. It is found that a pseudo-steady MR solution always exists for a given M_s for θ_w smaller than the limit determined by the von Neumann condition. Pseudo-steady MR solutions are first classified as backward- or forward-facing reflected oblique shock solutions. Both of the solutions can then be divided into three different types according to whether the reflected shock solution belongs to weak or strong oblique shock waves or if the flow downstream of the reflected shock is supersonic or subsonic, with the flow downstream of reflected strong oblique shocks always being subsonic.
机译:本文研究了伪稳态MR的三冲击理论激极解与γ= 1.4时M_s(入射冲击马赫数)和θ_w(反射楔角)初始条件的关系。讨论了满足正常马赫直杆边界条件的三震理论不同的拟稳态MR激振极点解。对于给定的M_s,对于小于von Neumann条件确定的极限的θ_w,始终存在伪稳态MR解。伪稳定MR解决方案首先分类为后向或前向反射斜向冲击解决方案。然后,根据反射激波解决方案属于弱斜波还是强斜激波,或者反射激波下游的流是超音速还是亚音速,而反射强激斜波的下游是流,则两种解决方案都可以分为三种类型。总是亚音速的

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