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Evaluation of Euler Fluxes for Hypersonic Heating Computations

机译:超音速加热计算的欧拉通量评估

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In hypersonic flow computations, it is a key issue to predict surface heating accurately, though this is still challenging because there always are possibilities of resulting in anomalous solutions. In this paper, three properties for flux functions are proposed: 1) shock stability/robustness, 2) conservation of total enthalpy, and 3) resolving boundary layer. Then, numerical experiments are performed for widely used or recently developed flux functions, and these fluxes are categorized into five major groups based on how they satisfy the three properties. These tests reveal that no flux function investigated here possesses all the three properties. In particular, the first one is not satisfied by any flux functions, including flux-vector-splittings. Finally, contributions of those properties are compared in a two-dimensional, viscous, hypersonic blunt-body problem. Results showed that the first and the third properties are crucial, and the second one is preferred to predict hypersonic heating. A group of flux functions that best satisfies these properties is suggested, and they are recommended either to be used or designed for hypersonic heating computations.
机译:在高超音速流计算中,准确预测表面加热是关键问题,尽管这仍然具有挑战性,因为总有可能导致异常解。本文提出了磁通函数的三个性质:1)冲击稳定性/鲁棒性; 2)总焓守恒; 3)解析边界层。然后,对广泛使用的或最近开发的磁通函数进行了数值实验,根据它们满足三种特性的方式,将这些磁通分为五类。这些测试表明,此处研究的通量函数均不具备这三个属性。特别是,第一个不满足于任何磁通函数,包括磁通矢量分裂。最后,在二维粘性高超声速钝体问题中比较了这些特性的贡献。结果表明,第一个和第三个特性至关重要,第二个特性更适合预测高超声速加热。建议使用一组最能满足这些特性的磁通函数,建议将其用于或设计用于超音速加热计算。

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