High-order compact gas-kinetic schemes for three-dimensional flow simulations on tetrahedral mesh
نویسندگان
چکیده
Abstract A general framework for the development of high-order compact schemes has been proposed recently. The core steps are composed following. 1). Based on a kinetic model equation, from generalized initial distribution flow variables construct time-accurate evolution solution gas function at cell interface and obtain corresponding flux function; 2). Introduce WENO-type weighting functions into time-derivative in multistage multi-derivative (MSMD) time stepping scheme to cope with possible impingement shock wave within step, update cell-averaged conservative inside each control volume; 3). Model both sides separately, take moments inner get variables, gradients 4). their gradients, develop data reconstruction condition distributions beginning next step. gas-kinetic (GKS) up sixth-order accuracy space fourth-order constructed 2D unstructured mesh. In this paper, GKS three-dimensional tetrahedral mesh will be further focus reconstruction. Nonlinear weights designed achieve smooth Navier-Stokes keep super robustness 3D computation strong interactions. uses large step CFL number 0.6 simulations subsonic hypersonic flow. series test cases used validate scheme. can applications complex geometry.
منابع مشابه
High-Order Flux Reconstruction Schemes for LES on Tetrahedral Meshes
The use of the high-order Flux Reconstruction (FR) spatial discretization scheme for LES on unstructured meshes is investigated. Simulations of the compressible Taylor-Green vortex at Re = 1600 demonstrate that the FR scheme has low numerical dissipation and accurately reproduces the turbulent energy cascade at low resolution, making it ideal for high-order LES. To permit the use of subgrid-sca...
متن کاملHigh Order Compact Finite Difference Schemes for Solving Bratu-Type Equations
In the present study, high order compact finite difference methods is used to solve one-dimensional Bratu-type equations numerically. The convergence analysis of the methods is discussed and it is shown that the theoretical order of the method is consistent with its numerical rate of convergence. The maximum absolute errors in the solution at grid points are calculated and it is shown that the ...
متن کاملHigh-Order Semi-Implicit Schemes for Unsteady Compressible Flow Simulations
Direct numerical simulation of stability and transition of compressible boundary layers requires high-orderaccurate and computationally ef cient numerical methods to resolve a wide range of timeand length scales associated with wave elds in the boundary layers. Explicit methods have been used mainly in such simulations to advance the compressible Navier–Stokes equations in time. However, the...
متن کاملA high-order gas-kinetic Navier-Stokes flow solver
The foundation for the development of modern compressible flow solver is based on the Riemann solution of the inviscid Euler equations. The high-order schemes are basically related to highorder spatial interpolation or reconstruction. In order to overcome the low-order wave interaction mechanism due to the Riemann solution, the temporal accuracy of the scheme can be improved through the Runge-K...
متن کاملThird Order WENO Scheme on Three Dimensional Tetrahedral Meshes
We extend the weighted essentially non-oscillatory (WENO) schemes on two dimensional triangular meshes developed in [7] to three dimensions, and construct a third order finite volume WENO scheme on three dimensional tetrahedral meshes. We use the Lax-Friedrichs monotone flux as building blocks, third order reconstructions made from combinations of linear polynomials which are constructed on div...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: Advances in Aerodynamics
سال: 2023
ISSN: ['2524-6992']
DOI: https://doi.org/10.1186/s42774-022-00132-y