Role of wall temperature on shock train in a rectangular isolator
Lu HB; Wang D; Chen X; Yue LJ(岳连捷)
2016
会议名称52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
会议日期July 25, 2016 - July 27, 2016
会议地点Salt Lake City, UT, United states
关键词Aero heating Dual mechanisms On flow Shock train Specific heat ratio Total pressure Total temperatures Wall temperatures
通讯作者Ji, Feng (yuelj@imech.ac.cn)
中文摘要Aimed at the problem of isolator being seriously heated by aeroheating at a long time fly, effects of wall temperature on flow characteristics and performance of isolator are experimentally and numerically investigated in detail under the different entrance conditions including total temperature and total pressure. The results show that shock train is affected by the dual mechanism of isolator wall temperature and airflow total temperature. With an increase of wall temperature and a reduction of total temperature, the length of shock train increases. This tendency can be characterized by the variation of shock train length with ratio of wall temperature to total temperature, viz., shock train length increases with ratio of wall temperature to total temperature. Based on the present data, both the ratio of wall temperature to total temperature and specific heat ratio are introduced to modify the correlation of Waltrup and Billig [5] for predicting shock train length of practical design with the coverage of more physical influencing factors. © 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
收录类别EI
会议网址10.2514/6.2016-4708
会议录52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
语种英语
ISBN号9781624104060
内容类型会议论文
源URL[http://dspace.imech.ac.cn/handle/311007/60149]  
专题力学研究所_高温气体动力学国家重点实验室
推荐引用方式
GB/T 7714
Lu HB,Wang D,Chen X,et al. Role of wall temperature on shock train in a rectangular isolator[C]. 见:52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. Salt Lake City, UT, United states. July 25, 2016 - July 27, 2016.10.2514/6.2016-4708.
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