![]() |
个人信息Personal Information
教授
博士生导师
硕士生导师
任职 : 国家重大专项专家组成员、教育部热防护专业组组长、国际华人计算力学协会理事、中国航空学会理事、中国航空学会强度与设计专业委员会委员、国际边界单元法协会会员、教育部高等学校航空航天类专业教学指导委员会委员
性别:男
毕业院校:Glasgow University
学位:博士
所在单位:力学与航空航天学院
办公地点:海宇楼403A
联系方式:0411-84706332
电子邮箱:xwgao@dlut.edu.cn
Radial integration BEM for dynamic coupled thermoelastic analysis under thermal shock loading
点击次数:
论文类型:期刊论文
发表时间:2015-10-01
发表刊物:COMPUTERS & STRUCTURES
收录刊物:SCIE、EI、Scopus
卷号:158
页面范围:140-147
ISSN号:0045-7949
关键字:Thermal shock; Dynamic coupled thermoelasticity; Radial integration BEM; Newmark method
摘要:In this paper, the radial integration boundary element method (RIBEM) is developed for two- and three-dimensional dynamic coupled thermoelastic analysis. Based on the classical thermoelasticity theory, boundary-domain integral equations for dynamic coupled thermoelastic problems are derived using the weighted residual method. The elastostatic and steady-state heat conduction fundamental solutions are employed in deriving the integral equations for dynamic coupled thermoelastic problems and this approach leads to domain integrals appearing in the resulting integral equations. The radial integral method (RIM) is employed to transform the domain integrals into boundary integrals and thus the boundary-only integral equations formulation can be achieved. It is then discretized into a system of time-dependent algebraic equations, which is solved by the standard Newmark time-integration scheme. Numerical results for several examples are given to demonstrate the efficiency and the accuracy of the present formulation. (C) 2015 Elsevier Ltd. All rights reserved.