IMECH-IR  > 高温气体动力学国家重点实验室
Role of wall temperature on shock train in a rectangular isolator
Lu HB; Wang D; Chen X; Yue LJ(岳连捷); Ji, Feng (yuelj@imech.ac.cn)
Source Publication52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
2016
Conference Name52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
Conference DateJuly 25, 2016 - July 27, 2016
Conference PlaceSalt Lake City, UT, United states
AbstractAimed 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.
KeywordAero Heating Dual Mechanisms On Flow Shock Train Specific Heat Ratio Total Pressure Total Temperatures Wall Temperatures
DepartmentLHD高超声速推进技术
ISBN9781624104060
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Indexed ByEI
Language英语
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/60149
Collection高温气体动力学国家重点实验室
Corresponding AuthorJi, Feng (yuelj@imech.ac.cn)
Recommended Citation
GB/T 7714
Lu HB,Wang D,Chen X,et al. Role of wall temperature on shock train in a rectangular isolator[C],2016.
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