Comparative study of different numerical approaches in space-time CESE framework for high-fidelity flow simulations

被引:2
作者
Cheng, Gary C. [1 ]
Venkatachari, Balaji Shankar [1 ]
Chang, Chau-Lyan [2 ]
Chang, Sin-Chung [3 ]
机构
[1] Univ Alabama Birmingham, Birmingham, AL 35294 USA
[2] NASA, Langley Res Ctr, Hampton, VA 23681 USA
[3] NASA, Glenn Res Ctr, Cleveland, OH 44135 USA
基金
美国国家航空航天局;
关键词
CFD; Space-time CESE method; Aeroacoustics; Hypersonic flows; Roughness element; SOLUTION ELEMENT METHOD; CONSERVATION ELEMENT; HIGH-RESOLUTION; NAVIER-STOKES; SCHEMES; EQUATIONS; LAWS;
D O I
10.1016/j.compfluid.2011.01.030
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
With the advancement of computer hardware, the trend of research in computational fluid dynamics is moving towards development of highly accurate, unstructured-mesh compatible, robust and efficient numerical methods for simulating problems involving strong transient effects and relatively complex geometries as well as physics. The space-time conservation element and solution element method is a genuinely multi-dimensional, unstructured-mesh compatible numerical framework, which was built from a consistent and synergetic integration of conservation laws in the space-time domain to avoid the limitations of conventional schemes, such as the use of 1-D flux reconstruction with a Riemann solver. It has been shown that the framework can be used for time-accurate simulations of a variety of problems involving unsteady waves, strong flow discontinuities, and their interactions with remarkable accuracy. However, this method at its current state has encountered the challenge in balancing the robustness and numerical accuracy when highly stretched meshes were used in viscous flow simulation. In this paper, we briefly discuss various numerical approaches developed for this framework thus far as well as their strengths and weaknesses, and conduct a comparative study of their numerical accuracies using some 2-D viscous benchmark test cases. The application of this method in realistic, complex 3-D problems is also included here to demonstrate its computational efficiency in large-scale computing. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:47 / 54
页数:8
相关论文
共 33 条
[1]  
[Anonymous], 1990, "Numerical Computation of Internal and External Flows"
[2]  
Atkins H.L., 2009, 20093787 AIAA
[3]   A high-order accurate discontinuous finite element method for the numerical solution of the compressible Navier-Stokes equations [J].
Bassi, F ;
Rebay, S .
JOURNAL OF COMPUTATIONAL PHYSICS, 1997, 131 (02) :267-279
[4]  
CHANG C. L., 2010, 20101572 AIAA
[5]   Hypersonic viscous flow over large roughness elements [J].
Chang, Chau-Lyan ;
Choudhari, Meelan M. .
THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 2011, 25 (1-4) :85-104
[6]  
CHANG CL, 2007, 20075818 AIAA
[7]  
Chang S. C., 2003, AIAA Paper 2003-5285.
[8]  
Chang S.C., 2010, 2010543 AIAA
[9]   The space-time conservation element and solution element method: A new high-resolution and genuinely multidimensional paradigm for solving conservation laws [J].
Chang, SC ;
Wang, XY ;
Chow, CY .
JOURNAL OF COMPUTATIONAL PHYSICS, 1999, 156 (01) :89-136
[10]   Application of the space-time conservation element and solution element method to one-dimensional convection-diffusion problems [J].
Chang, SC ;
Wang, XY ;
To, WM .
JOURNAL OF COMPUTATIONAL PHYSICS, 2000, 165 (01) :189-215