The Effects of Insulation thickness on Heat Transfer for Thermal Protection System

摘要：

The effects of insulation thickness are investigated with potential application in thermal protection system of hypersonic and re-entry vehicles. The traditional thermal protection system is modeled by the finite difference approach. Four different thicknesses of insulations’ TPS are studied. The numerical calculation results show that structure temperature decreases as the insulation thickness increases as well as temperature difference increases, however, this effect weakens as the insulation thickness increased.

作者: Shuang Liu Boming Zhang Weihua Xie

作者单位: Composite material and structure,Harbin Institute of Technology,Harbin,150080,China.

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 383-388

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）