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Simulation of high-speed flows by an unstructured grid implicit method including real gas effects

机译:通过非结构化网格隐式方法模拟高速流动,包括真实气体效应

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摘要

The incorporation of real gas effects into an efficient dual-time implicit method is presented for numerical simulation of high-speed flows. Two-dimensional compressible Navier-Stokes equations are discretized by an implicit approach in a real-time basis. The resulting set of implicit nonlinear equations is then solved iteratively in pseudo-time using a Runge-Kutta scheme. A control-volume central difference approach is used for spatial discretization on unstructured grids. For an equilibrium chemically reacting air, simplified equations are used to calculate the thermodynamics and transport properties of equilibrium air. The method is applied to hypersonic laminar flows of air over a compression ramp and a circular cylinder. Computational results are compared with those of other numerical methods and experimental data. Excellent agreement is obtained for various flow and heat transfer characteristics. Considerable reduction in computational time has also been achieved compared with the original explicit method.
机译:为高速流动的数值模拟提供了实际气体效应将实际气体效应纳入了高效的双时隐式方法。二维可压缩Navier-Stokes方程在实时采用隐式方法离散化。然后使用Runge-Kutta方案迭代地解决所得到的隐式非线性方程组。控制卷中央差异方法用于非结构化网格上的空间离散化。对于平衡化学反应空气,简化的方程用于计算平衡空气的热力学和运输特性。该方法应用于压缩斜坡和圆柱上的空气的高超声声层流。将计算结果与其他数值方法和实验数据进行比较。为各种流动和传热特性获得了优异的一致性。与原始显式方法相比,计算时间的相当大的计算时间也得到了相当大的降低。

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