个人信息Personal Information
特聘研究员
博士生导师
硕士生导师
任职 : 空气动力学会委员会委员;国家重大科技工程专项气动力/热专家组成员;《空气动力学报》编委;《气体物理》编委;
性别:男
毕业院校:中国空气动力研究与发展中心
学位:博士
所在单位:力学与航空航天学院
学科:飞行器设计. 流体力学
办公地点:大连理工大学综合实验一号楼203
联系方式:0411-84707176
电子邮箱:liujun65@dlut.edu.cn
Evaluation of rotated upwind schemes for contact discontinuity and strong shock
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论文类型:期刊论文
发表时间:2016-08-01
发表刊物:COMPUTERS & FLUIDS
收录刊物:SCIE、EI、Scopus
卷号:134
页面范围:11-22
ISSN号:0045-7930
关键字:Rotated upwind scheme; Carbuncle phenomenon; Shock-capturing; Dissipative density term; Contact discontinuity; Rotation strategy
摘要:Rotated upwind schemes have been evaluated as carbuncle-free shock-capturing methods. In order to reveal the relation between the rotated upwind-differencing direction and the performance of rotated upwind schemes, theoretical and numerical investigations are made. Three commonly used upwind schemes, including Roe scheme, AUSM(+) scheme and Van Leer scheme are investigated. According to the theoretical analysis, the dissipative terms of each upwind scheme are changed by the rotation procedure. Especially, the dissipative density term in the numerical flux function of rotated upwind schemes introduces extra dissipation. The numerical cases include simulations of laminar boundary layer, steady twin vortices and strong shock. The numerical results show that the carbuncle phenomenon can be eliminated by rotated upwind schemes, and the contact resolving capability of rotated upwind schemes is deteriorated by the rotation procedure. Monotonicity of the dissipation with rotation angle is also shown in the numerical results. Therefore, a novel rotation strategy that defines the rotation angle by a pressure weight function is introduced for tuning the dissipative effects adaptively. This strategy shows not only carbuncle-free result in hypersonic inviscid flow simulations, but also accurate results in viscous flow simulations. (C) 2016 Elsevier Ltd. All rights reserved.