An inverse Lax-Wendroff procedure for hyperbolic conservation laws with changing wind direction on the boundary
被引:18
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作者:
Lu, Jianfang
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机构:
South China Normal Univ, South China Res Ctr Appl Math & Interdisciplinary, Guangzhou 510631, Guangdong, Peoples R ChinaSouth China Normal Univ, South China Res Ctr Appl Math & Interdisciplinary, Guangzhou 510631, Guangdong, Peoples R China
Lu, Jianfang
[1
]
Shu, Chi-Wang
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机构:
Brown Univ, Div Appl Math, Providence, RI 02912 USASouth China Normal Univ, South China Res Ctr Appl Math & Interdisciplinary, Guangzhou 510631, Guangdong, Peoples R China
Shu, Chi-Wang
[2
]
Tan, Sirui
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机构:
Brown Univ, Div Appl Math, Providence, RI 02912 USASouth China Normal Univ, South China Res Ctr Appl Math & Interdisciplinary, Guangzhou 510631, Guangdong, Peoples R China
Tan, Sirui
[2
]
Zhang, Mengping
论文数: 0引用数: 0
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机构:
Univ Sci & Technol China, Sch Math Sci, Hefei 230026, Anhui, Peoples R ChinaSouth China Normal Univ, South China Res Ctr Appl Math & Interdisciplinary, Guangzhou 510631, Guangdong, Peoples R China
Zhang, Mengping
[3
]
机构:
[1] South China Normal Univ, South China Res Ctr Appl Math & Interdisciplinary, Guangzhou 510631, Guangdong, Peoples R China
[2] Brown Univ, Div Appl Math, Providence, RI 02912 USA
[3] Univ Sci & Technol China, Sch Math Sci, Hefei 230026, Anhui, Peoples R China
In this paper, we reconsider the inverse Lax-Wendroff (ILW) procedure, which is a numerical boundary treatment for solving hyperbolic conservation laws, and propose a new approach to evaluate the values on the ghost points. The ILW procedure was firstly proposed to deal with the "cut cell" problems, when the physical boundary intersects with the Cartesian mesh in an arbitrary fashion. The key idea of the ILW procedure is repeatedly utilizing the partial differential equations (PDEs) and inflow boundary conditions to obtain the normal derivatives of each order on the boundary. A simplified ILW procedure was proposed in [28] and used the ILW procedure for the evaluation of the first order normal derivatives only. The main difference between the simplified ILW procedure and the proposed ILW procedure here is that we define the unknown u and the flux f(u) on the ghost points separately. One advantage of this treatment is that it allows the eigenvalues of the Jacobian f'(u) to be close to zero on the boundary, which may appear in many physical problems. We also propose a new weighted essentially non-oscillatory (WENO) type extrapolation at the outflow boundaries, whose idea comes from the multi-resolution WENO schemes in [32]. The WENO type extrapolation maintains high order accuracy if the solution is smooth near the boundary and it becomes a low order extrapolation automatically if a shock is close to the boundary. This WENO type extrapolation preserves the property of self-similarity, thus it is more preferable in computing the hyperbolic conservation laws. We provide extensive numerical examples to demonstrate that our method is stable, high order accurate and has good performance for various problems with different kinds of boundary conditions including the solid wall boundary condition, when the physical boundary is not aligned with the grids. (C) 2020 Elsevier Inc. All rights reserved.
机构:
KTH Royal Inst Technol, Linne FLOW Ctr, Dept Math, S-10044 Stockholm, SwedenKTH Royal Inst Technol, Linne FLOW Ctr, Dept Math, S-10044 Stockholm, Sweden
Liu, Shihao
Li, Tingting
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机构:
Henan Univ, Sch Math & Stat, Kaifeng 475004, Henan, Peoples R ChinaKTH Royal Inst Technol, Linne FLOW Ctr, Dept Math, S-10044 Stockholm, Sweden
Li, Tingting
Cheng, Ziqiang
论文数: 0引用数: 0
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机构:
Hefei Univ Technol, Sch Math, Hefei 230026, Anhui, Peoples R ChinaKTH Royal Inst Technol, Linne FLOW Ctr, Dept Math, S-10044 Stockholm, Sweden
Cheng, Ziqiang
Jiang, Yan
论文数: 0引用数: 0
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机构:
Univ Sci & Technol China, Sch Math Sci, Hefei 230026, Anhui, Peoples R ChinaKTH Royal Inst Technol, Linne FLOW Ctr, Dept Math, S-10044 Stockholm, Sweden
Jiang, Yan
Shu, Chi-Wang
论文数: 0引用数: 0
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机构:
Brown Univ, Div Appl Math, Providence, RI 02912 USAKTH Royal Inst Technol, Linne FLOW Ctr, Dept Math, S-10044 Stockholm, Sweden
Shu, Chi-Wang
Zhang, Mengping
论文数: 0引用数: 0
h-index: 0
机构:
Univ Sci & Technol China, Sch Math Sci, Hefei 230026, Anhui, Peoples R ChinaKTH Royal Inst Technol, Linne FLOW Ctr, Dept Math, S-10044 Stockholm, Sweden
机构:
Natl Univ Def Technol, Coll Liberal Arts & Sci, Changsha 410073, Peoples R ChinaNatl Univ Def Technol, Coll Liberal Arts & Sci, Changsha 410073, Peoples R China
Hao, Tianchu
Chen, Yaming
论文数: 0引用数: 0
h-index: 0
机构:
Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Peoples R ChinaNatl Univ Def Technol, Coll Liberal Arts & Sci, Changsha 410073, Peoples R China
Chen, Yaming
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机构:
Tang, Lingyan
Song, Songhe
论文数: 0引用数: 0
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机构:
Natl Univ Def Technol, Coll Liberal Arts & Sci, Changsha 410073, Peoples R ChinaNatl Univ Def Technol, Coll Liberal Arts & Sci, Changsha 410073, Peoples R China
机构:
Univ Estado Rio De Janeiro, Math & Stat Inst, Rio De Janeiro, BrazilUniv Estado Rio De Janeiro, Math & Stat Inst, Rio De Janeiro, Brazil
Borges, Rafael B. de Rezende
da Silva, Nicholas Dicati P.
论文数: 0引用数: 0
h-index: 0
机构:
Univ Fed Parana, Lab Numer Experimentat, Dept Mech Engn, Curitiba, Parana, BrazilUniv Estado Rio De Janeiro, Math & Stat Inst, Rio De Janeiro, Brazil
da Silva, Nicholas Dicati P.
Gomes, Francisco A. A.
论文数: 0引用数: 0
h-index: 0
机构:
Univ Tecnol Fed Parana, Dept Mech Engn, Pato Branco, BrazilUniv Estado Rio De Janeiro, Math & Stat Inst, Rio De Janeiro, Brazil
Gomes, Francisco A. A.
Shu, Chi-Wang
论文数: 0引用数: 0
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机构:
Brown Univ, Div Appl Math, Providence, RI 02912 USAUniv Estado Rio De Janeiro, Math & Stat Inst, Rio De Janeiro, Brazil
Shu, Chi-Wang
Tan, Sirui
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机构:
Brown Univ, Div Appl Math, Providence, RI 02912 USAUniv Estado Rio De Janeiro, Math & Stat Inst, Rio De Janeiro, Brazil
机构:Nanjing University of Aeronautics and Astronautics,Key Laboratory of Mathematical Modelling and High Performance Computing of Air Vehicles (NUAA), MIIT
Liang Li
Jun Zhu
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机构:Nanjing University of Aeronautics and Astronautics,Key Laboratory of Mathematical Modelling and High Performance Computing of Air Vehicles (NUAA), MIIT
Jun Zhu
Chi-Wang Shu
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机构:Nanjing University of Aeronautics and Astronautics,Key Laboratory of Mathematical Modelling and High Performance Computing of Air Vehicles (NUAA), MIIT
Chi-Wang Shu
Yong-Tao Zhang
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机构:Nanjing University of Aeronautics and Astronautics,Key Laboratory of Mathematical Modelling and High Performance Computing of Air Vehicles (NUAA), MIIT
Yong-Tao Zhang
[J].
Communications on Applied Mathematics and Computation,
2023,
5
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