Numerical Simulation of Couple Aerodynamic Heating and Structural Conduction for a Hypersonic Vehicle (IWAE2008)

摘要：

A method of thermal coupled between the flow and the structural for 3-Dimension model is put forward in this paper. Solve the N-S equation by using finite volume which was put forward by Jameson and the finite element software ANSYS is used for solving the heat conduction equation. Coupling time step and convergence criterions for flow field calculation are studied for getting accurate prediction of the aerothermal loads and save time for calculation.

关键词： aerodynamic heating numerical simulation hypersonic

作者: Fu Zhiyong Liu Hong

作者单位: School of Naval Architecture, Ocean and Civil Engineering, Shanghai Jiaotong University, Shanghai,20 Department of Engineering Mechanics, Shanghai Jiaotong University, Shanghai, 200240 PR China

会议类型: 国际会议

会议名称: 2008 National Academic Symposium for Ph. D. Candidates and Tri-University Workshop on Aero-Structural Mechanics & Aerospace Engineering(NASPCTUWMAE2008)(2008年国际航天航空工程会议暨2008年博士生学术会议(力学))

会议地点: 北京

会议语种:英文

页码: 1-4

在线出版日期: 2008-10-23（万方平台首次上网日期，不代表论文的发表时间）