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Numerical investigation of buoyancy-driven compressible laminar flow using new method preconditioned all-speed roe scheme

机译:浮力驱动可压缩层流的新方法预处理全速鱼卵方案的数值研究

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In this study, numerical simulation is performed with a focus on the application of new modified preconditioned all-speed Roe scheme to simulate natural convection flows. The new modified preconditioned all-speed Roe Scheme primarily utilizes the local flow parameters for calculation of the coefficients of numerator in dissipation term of the scheme instead of using the global cut-off Mach number strategy (which is advantageous for natural convection flows) and has been shown to have better accuracy than preconditioned Roe Scheme for Low Mach number flows. For the present simulation, the compressible governing equation in conservation form, new modified preconditioned all-speed Roe scheme and dual time stepping are employed. The validation of numerical algorithm is divided into two investigations a) natural convection flow within differentially heated enclosed square cavity and b) open-ended vertical channel asymmetrically heated for a wide range of Rayleigh number with air (Pr 0.72) as working fluid. Visualization of fluid flow dynamics conducted for both classes of geometries for all range of Rayleigh number show similar phenomena in accordance with previous literatures and compared data also show very good agreement with previous literatures. All results indicate that the new modified preconditioned all-speed Roe scheme is very much competent and accurate for simulation of buoyancy induced compressible convection flows without relying on the correct prediction of global cut-off Mach number.
机译:在这项研究中,数值模拟的重点是应用新的改进的预处理全速Roe方案来模拟自然对流。新的改进的预处理全速Roe方案主要利用局部流量参数来计算方案耗散项下的分子系数,而不是使用全局截止马赫数策略(这对自然对流有利),并且具有结果表明,对于低马赫数流,该算法比预处理Roe方案具有更高的准确性。对于当前的仿真,采用守恒形式的可压缩控制方程,新的改进的预处理全速Roe方案和双时间步长。数值算法的验证分为两个研究:a)差热封闭的方腔内的自然对流流动; b)以大范围的瑞利数以空气(Pr 0.72)作为工作流体不对称加热的开放式垂直通道。根据以前的文献,针对两种几何类型的所有瑞利数范围进行的流体流动动力学的可视化显示出相似的现象,并且比较的数据也显示出与先前的文献非常吻合。所有结果表明,新的改进的预调节全速Roe方案非常有能力且准确地模拟浮力引起的可压缩对流,而无需依赖于全球临界马赫数的正确预测。

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