Optimization design of the rocket launching facilities and the thermal protection

摘要：

Based on fully hexahedral mesh and the k-e turbulence model, the computational fluid dynamics method was used to the numerical simulation. Different angle of the double-faced deflector and the thermal protection of the launching facilities were calculated. The pressure and temperature parameters were obtained and the result was compared and analyzed. The appropriate model was selected. The numerical calculation method and the results can be used to the engineering.

关键词： rocket plume launching facilities numerical simulation thermal protection deflector

作者: JIANG Yi MA Yan-li WANG Wei-chen HAO Ji-guang

作者单位: Department of Aerospace Engineering,Beijing Institute of Technology Beijing,China

会议类型: 国际会议

会议名称: The 2nd IEEE International Conference on Advanced Computer Control(第二届先进计算机控制国际会议 ICACC 2010)

会议地点: 沈阳

会议语种:英文

页码: 30-33

在线出版日期: 2010-03-27（万方平台首次上网日期，不代表论文的发表时间）