A high order boundary scheme to simulate complex moving rigid body under impingement of shock wave

被引:7
|
作者
Cheng, Ziqiang [1 ]
Liu, Shihao [1 ]
Jiang, Yan [1 ]
Lu, Jianfang [2 ]
Zhang, Mengping [1 ]
Zhang, Shuhai [3 ]
机构
[1] Univ Sci & Technol China, Sch Math Sci, Hefei 230026, Peoples R China
[2] South China Normal Univ, South China Res Ctr Appl Math & Interdisciplinary, Guangzhou 510631, Peoples R China
[3] China Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Sichuan, Peoples R China
基金
中国国家自然科学基金;
关键词
inverse Lax-Wendroff (ILW) procedure; complex moving boundary scheme; Cartesian mesh; high order accuracy; compressible inviscid shock wave; O242; EFFICIENT IMPLEMENTATION; DIFFERENCE APPROXIMATIONS; STABILITY ANALYSIS; FLOWS;
D O I
10.1007/s10483-021-2735-7
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
In the paper, we study a high order numerical boundary scheme for solving the complex moving boundary problem on a fixed Cartesian mesh, and numerically investigate the moving rigid body with the complex boundary under the impingement of an inviscid shock wave. Based on the high order inverse Lax-Wendroff (ILW) procedure developed in the previous work (TAN, S. and SHU, C. W. A high order moving boundary treatment for compressible inviscid flows. Journal of Computational Physics, 230(15), 6023-6036 (2011)), in which the authors only considered the translation of the rigid body, we consider both translation and rotation of the body in this paper. In particular, we reformulate the material derivative on the moving boundary with no-penetration condition, and the newly obtained formula plays a key role in the proposed algorithm. Several numerical examples, including cylinder, elliptic cylinder, and NACA0012 airfoil, are given to indicate the effectiveness and robustness of the present method.
引用
收藏
页码:841 / 854
页数:14
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