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Analytical study for hypersonic flow past an elliptic cone with longitudinal curvature

机译:高超音速流经纵向曲率的椭圆锥的解析研究

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For hypersonic flow past an elliptic cone with longitudinal curvature, the outer-expansion analysis of shock layer and the inner-expansion analysis of the vortical layer are two major subjects of this study. ^The zeroth-order approximation of hypersonic conical flow obtained by nonlinear asymptotic theory is chosen as the basic-cone solution for the outer and inner expansions. ^In the outer analysis of the shock layer, the complicated governing equation of the outer flow field can be simplified by the appropriate approximation scheme, and the first-order approximations of properties are derived. ^In accordance with the asymptotic matching principle, the uniformly-valid approximation can be obtained and expressed in closed form. ^It is verified that the perturbation pressure and azimuthal velocity from outer solutions are actually the perturbation expansion values from inner solutions. ^Analysis of inner solutions illustrates the rapid variations on entropy and density of the vortical layer. ^(Author)
机译:对于经过具有纵向曲率的椭圆锥的高超声速流动,激波层的外扩展分析和涡旋层的内扩展分析是本研究的两个主要主题。 ^通过非线性渐近理论获得的高超音速圆锥形流的零阶近似被选作内外膨胀的基本锥解。 ^在冲击层的外部分析中,可以通过适当的近似方案简化外部流场的复杂控制方程,并推导特性的一阶近似。 ^根据渐近匹配原理,可以获得一致有效的近似值,并用封闭形式表示。 ^证实了外部溶液的摄动压力和方位角速度实际上是内部溶液的摄动膨胀值。 ^内部解决方案的分析说明了涡旋层的熵和密度的快速变化。 ^(作者)

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