High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model | |
Yang L1,2; 岳连捷2,3![]() ![]() ![]() | |
Source Publication | Journal of Physics: Conference Series |
2020-07-01 | |
Pages | 10.1088/1742-6596/1600/1/012024 |
Conference Name | 4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020, |
Conference Date | June 27, 2020 - June 28, 2020 |
Conference Place | Asian Union of Information Technology |
Abstract | The goal of this paper is to implement an accurate and robust solver for compressible Navier-Stokes equations coupled with the Spalart–Allmaras model, which possesses the capability of shock-capturing and predication of boundary layer and separated flow. In a given stencil width, a WENO-Z scheme equipped with Roe flux difference split method is used to calculate the inviscid flux, and central differencing scheme for the viscous terms are employed. The explicit Runge-Kutta is adopted for the temporal discretization. The simulation results of selected cases are given to verify the validation of the solver. |
WOS ID | WOS:000615694800024 |
Indexed By | EI ; CPCI-S |
Language | 英语 |
Citation statistics | |
Document Type | 会议论文 |
Identifier | http://dspace.imech.ac.cn/handle/311007/85557 |
Collection | 高温气体动力学国家重点实验室 |
Affiliation | 1.School of Aerospace Engineering, Beijing Institute of Technology, Beijing, 100081, China 2.State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing, 100190, China 3.School of Engineering Sciences, University of Chinese Academy of Sciences, Beijing, 100049, China |
Recommended Citation GB/T 7714 | Yang L,岳连捷,张启帆,等. High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model[C]Journal of Physics: Conference Series,2020:10.1088/1742-6596/1600/1/012024. |
Files in This Item: | Download All | |||||
File Name/Size | DocType | Version | Access | License | ||
1600_012024.pdf(1289KB) | 会议论文 | 开放获取 | CC BY-NC-SA | View Download |
Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.
Edit Comment