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Gas kinetic flux solver based finite volume weighted essentially non-oscillatory scheme for inviscid compressible flows
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作者 Lan JIANG Jie WU +1 位作者 Liming YANG Hao DONG 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2023年第6期961-980,共20页
A high-order gas kinetic flux solver(GKFS)is presented for simulating inviscid compressible flows.The weighted essentially non-oscillatory(WENO)scheme on a uniform mesh in the finite volume formulation is combined wit... A high-order gas kinetic flux solver(GKFS)is presented for simulating inviscid compressible flows.The weighted essentially non-oscillatory(WENO)scheme on a uniform mesh in the finite volume formulation is combined with the circular function-based GKFS(C-GKFS)to capture more details of the flow fields with fewer grids.Different from most of the current GKFSs,which are constructed based on the Maxwellian distribution function or its equivalent form,the C-GKFS simplifies the Maxwellian distribution function into the circular function,which ensures that the Euler or Navier-Stokes equations can be recovered correctly.This improves the efficiency of the GKFS and reduces its complexity to facilitate the practical application of engineering.Several benchmark cases are simulated,and good agreement can be obtained in comparison with the references,which demonstrates that the high-order C-GKFS can achieve the desired accuracy. 展开更多
关键词 circular function-based gas kinetic flux solver(C-GKFS) weighted essentially non-oscillatory(weno)scheme compressible flow finite volume method
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Sparse-Grid Implementation of Fixed-Point Fast Sweeping WENO Schemes for Eikonal Equations
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作者 Zachary M.Miksis Yong-Tao Zhang 《Communications on Applied Mathematics and Computation》 EI 2024年第1期3-29,共27页
Fixed-point fast sweeping methods are a class of explicit iterative methods developed in the literature to efficiently solve steady-state solutions of hyperbolic partial differential equations(PDEs).As other types of ... Fixed-point fast sweeping methods are a class of explicit iterative methods developed in the literature to efficiently solve steady-state solutions of hyperbolic partial differential equations(PDEs).As other types of fast sweeping schemes,fixed-point fast sweeping methods use the Gauss-Seidel iterations and alternating sweeping strategy to cover characteristics of hyperbolic PDEs in a certain direction simultaneously in each sweeping order.The resulting iterative schemes have a fast convergence rate to steady-state solutions.Moreover,an advantage of fixed-point fast sweeping methods over other types of fast sweeping methods is that they are explicit and do not involve the inverse operation of any nonlinear local system.Hence,they are robust and flexible,and have been combined with high-order accurate weighted essentially non-oscillatory(WENO)schemes to solve various hyperbolic PDEs in the literature.For multidimensional nonlinear problems,high-order fixed-point fast sweeping WENO methods still require quite a large amount of computational costs.In this technical note,we apply sparse-grid techniques,an effective approximation tool for multidimensional problems,to fixed-point fast sweeping WENO methods for reducing their computational costs.Here,we focus on fixed-point fast sweeping WENO schemes with third-order accuracy(Zhang et al.2006[41]),for solving Eikonal equations,an important class of static Hamilton-Jacobi(H-J)equations.Numerical experiments on solving multidimensional Eikonal equations and a more general static H-J equation are performed to show that the sparse-grid computations of the fixed-point fast sweeping WENO schemes achieve large savings of CPU times on refined meshes,and at the same time maintain comparable accuracy and resolution with those on corresponding regular single grids. 展开更多
关键词 Fixed-point fast sweeping methods weighted essentially non-oscillatory(weno)schemes Sparse grids Static Hamilton-Jacobi(H-J)equations Eikonal equations
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New High-Order Numerical Methods for Hyperbolic Systems of Nonlinear PDEs with Uncertainties
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作者 Alina Chertock Michael Herty +3 位作者 Arsen S.Iskhakov Safa Janajra Alexander Kurganov Maria Lukacova-Medvid'ova 《Communications on Applied Mathematics and Computation》 EI 2024年第3期2011-2044,共34页
In this paper,we develop new high-order numerical methods for hyperbolic systems of nonlinear partial differential equations(PDEs)with uncertainties.The new approach is realized in the semi-discrete finite-volume fram... In this paper,we develop new high-order numerical methods for hyperbolic systems of nonlinear partial differential equations(PDEs)with uncertainties.The new approach is realized in the semi-discrete finite-volume framework and is based on fifth-order weighted essentially non-oscillatory(WENO)interpolations in(multidimensional)random space combined with second-order piecewise linear reconstruction in physical space.Compared with spectral approximations in the random space,the presented methods are essentially non-oscillatory as they do not suffer from the Gibbs phenomenon while still achieving high-order accuracy.The new methods are tested on a number of numerical examples for both the Euler equations of gas dynamics and the Saint-Venant system of shallow-water equations.In the latter case,the methods are also proven to be well-balanced and positivity-preserving. 展开更多
关键词 Hyperbolic conservation and balance laws with uncertainties Finite-volume methods Central-upwind schemes weighted essentially non-oscillatory(weno)interpolations
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二维进气道不启动流场非定常特性的混合LES/RANS模拟 被引量:1
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作者 陈逖 刘卫东 范晓樯 《航空动力学报》 EI CAS CSCD 北大核心 2012年第8期1792-1800,共9页
采用一种混合大涡模拟/雷诺平均Navier-Stokes(LES/RANS)方程模拟方法结合5阶WENO(weighted essentially non-oscillatory)格式对马赫数为3的来流中、内收缩比为1.5的不启动状态下的二维进气道进行了计算,再现了不启动进气道中的非定常... 采用一种混合大涡模拟/雷诺平均Navier-Stokes(LES/RANS)方程模拟方法结合5阶WENO(weighted essentially non-oscillatory)格式对马赫数为3的来流中、内收缩比为1.5的不启动状态下的二维进气道进行了计算,再现了不启动进气道中的非定常流场.计算结果表明:所采用的模拟方法对入口处的平均绝热壁温、摩擦速度和雷诺应力的计算精度较好,进气道不启动流场中激波波系和分离区存在大时空尺度的低频运动,其占主导的特征频率和典型的激波/湍流边界层干扰问题中激波和分离区的低频频率接近,且进气道出现了间歇性的启动状态. 展开更多
关键词 混合大涡/雷诺平均Navier-Stokes方程模拟方法 声速喷流 “回收/调节”方法 weno(weighted essentially non—oscillatory)格式 二维进气道
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