Interface flux reconstruction method based on optimized weight essentially non-oscillatory scheme

作者：Peixun Yu, Junqiang Bai, Hai Li Yang, Song Chen, Kai Pan · 发表于：Chinese Journal of Aeronautics · 年份：2018 · DOI：10.1016/j.cja.2018.02.012 · 被引用次数：7 · 研究领域：Computational Fluid Dynamics and Aerodynamics、Aerodynamics and Acoustics in Jet Flows、Fluid Dynamics and Turbulent Flows

Aimed at the computational aeroacoustics multi-scale problem of complex configurations discretized with multi-size mesh, the flux reconstruction method based on modified Weight Essentially Non-Oscillatory (WENO) scheme is proposed at the interfaces of multi-block grids. With the idea of Dispersion-Relation-Preserving (DRP) scheme, different weight coefficients are obtained by optimization, so that it is in WENO schemes with various characteristics of dispersion and dissipation. On the basis, hybrid flux vector splitting method is utilized to intelligently judge the amplitude of the gap between grid interfaces. After the simulation and analysis of 1D convection equation with different initial conditions, modified WENO scheme is proved to be able to independently distinguish the gap amplitude and generate corresponding dissipation according to the grid resolution. Using the idea of flux reconstruction at grid interfaces, modified WENO scheme with increasing dissipation is applied at grid points, while DRP scheme with low dispersion and dissipation is applied at the inner part of grids. Moreover, Gauss impulse spread and periodic point sound source flow among three cylinders with multi-scale grids are carried out. The results show that the flux reconstruction method at grid interfaces is capable of dealing with Computational AeroAcoustics (CAA) multi-scale problems.