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
An adaptive discontinuity fitting technique on unstructured dynamic grids
点击次数:
论文类型:期刊论文
发表时间:2021-01-09
发表刊物:SHOCK WAVES
卷号:29
期号:8,SI
页面范围:1103-1115
ISSN号:0938-1287
关键字:Shock fitting; Unstructured dynamic grids; Supersonic flow; Shock interactions
摘要:A novel, adaptive discontinuity fitting technique has been further developed on unstructured dynamic grids to fit both shock waves and contact discontinuities in steady flows. Moreover, in order to efficiently obtain shock-fitting solutions, two strategies, direct-fitting and indirect-fitting, have been proposed to, respectively, deal with simple and complex flows. More specifically, without first computing the flow field by a shock-capturing method, the direct-fitting strategy, mainly dealing with these discontinuities of which topologies are clearly known, can quickly obtain the solutions by initially presetting an approximate discontinuity front. By contrast, the indirect-fitting strategy, especially in coping with the complicated discontinuity structures, must utilize both shock-capturing solutions and shock detection techniques to first determine initial discontinuity locations. The two strategies have been successfully applied to a series of compressible flows, including a two-dimensional flow with type IV shock-shock interaction and a three-dimensional flow with type VI interaction. In addition, comparing the fully-fitting solution with the partially-fitting solution in the discontinuity interaction region, it is indicated that an accurate result can be acquired if all the discontinuities in the vicinity of interaction points are fully fitted. Nevertheless, the computational accuracy of expansion waves can indeed significantly affect the downstream discontinuities.