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MC-Smooth: A Mass-Conserving, Smooth Vorticity-Velocity Formulation for Multidimensional Flows

机译:MC-平滑:用于多维流动的质量保守,平稳的涡流 - 速度配方

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In this study, a novel vorticity-velocity formulation - the Mass-Conserving, Smooth (MC-Smooth) formulation - is developed. Compared to some existing vorticity-velocity formulations, MC-Smooth is appealing because it can generate smooth and mass-conservative solutions without employing staggered grids. Furthermore, MC-Smooth can preserve ellipticity and favorable convergence properties of the governing equations and does not require follow-up simulations (e.g., replacing one of the equations with continuity and then recon-verging). The performance of MC-Smooth is compared with that of two vorticity-velocity formulations from the literature for three test cases: a laminar jet of air with an inhomogeneous density field and two laminar methane/air flames with detailed chemistry. Since each test problem is either axisymmetric or two-dimensional (2D) planar, a 2D computational domain with a nonuniform grid was employed. The governing equations and boundary conditions were discretized on the mesh by a finite difference approach, and the resulting set of nonlinear equations was solved by a damped, modified Newton's method. By comparing the performance of each vorticity-velocity formulation without any follow-up simulations, MC-Smooth is shown to generate more physically accurate results by ensuring both mass conservation and smoothness of the velocity field.
机译:在该研究中,开发了一种新型涡流 - 速度配方 - 显影,平稳(MC-光滑)制剂。与一些现有的涡流 - 速度配方相比,MC-Shable非常有吸引力,因为它可以产生光滑和质量保守的解决方案而不采用交错网格。此外,MC-Smovelt可以保留控制方程的椭圆性和有利的收敛性,并且不需要随访模拟(例如,用连续性替换其中一个方程然后重新登录)。将MC-平滑的性能与三个测试用例的文献中的两个涡流速度制剂进行了比较:空气的层流射流,其中具有非均匀密度场和具有详细化学的两个层状甲烷/空气火焰。由于每个测试问题是轴对称或二维(2D)平面,所以采用具有非均匀网格的2D计算域。通过有限差异方法将控制方程和边界条件离散化,并通过阻尼修正的牛顿的方法解决了所得的非线性方程组。通过在没有任何后续模拟的情况下比较每个涡流 - 速度制剂的性能,显示MC-Smovelt通过确保速度场的质量保护和平滑度来产生更具物理准确的结果。

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