Simulation on the Transient Temperature Field of Turbine Disk

摘要：

The distribution of the temperature field for the turbine disk of the rocket engine is studied using finite element method. The simplified model of the turbine disk is firstly built. Then the transient temperature for the turbine disk is calculated. Results show that the distribution of the temperature is in changing state. Tt is also indicated that th? research on the temperature distribution of the disk is meaningful.

关键词： Temperature distribution Turbine disk Transient temperature

作者: Song Shaowei Li Feng He Zexia

作者单位: College of Astronautics,Northwestern Ploytechnical University,Xian 710072,China Xian Aerospace Propulsion Institute,Xian 710100,China

会议类型: 国际会议

会议名称: 2011 International Conference on Opto-Electronics Engineering and Information Science(2011光电电子工程与信息科学国际会议 ICOEIS 2011)

会议地点: 西安

会议语种:英文

页码: 1394-1396

在线出版日期: 2011-12-23（万方平台首次上网日期，不代表论文的发表时间）