Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers
文献类型:期刊论文
作者 | Yue LJ(岳连捷)![]() ![]() ![]() |
刊名 | AEROSPACE SCIENCE AND TECHNOLOGY
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出版日期 | 2018-03-01 |
卷号 | 74页码:72-80 |
关键词 | Inlet restart Cowl shock Shock wave boundary layer interactions |
ISSN号 | 1270-9638 |
DOI | 10.1016/j.ast.2017.12.018 |
英文摘要 | The effect of cowl angle on the restart characteristics of simple ramp type hypersonic inlets was experimentally investigated in shock tunnel equipped with schlieren imagery and static pressure measurement. The cowl shock strength is found to be a key factor that determines the inlet restart and makes the restart contraction ratios significantly deviate from the Kantrowitz criterion. Stronger cowl shock tends to degrade the inlet restart capability by causing larger separation bubble and higher pressure loss during the restarting process. In particular, a sensitive range of the cowl angles, within which the restart contraction ratio decreases rapidly, was identified. A design concept of multiple noncoalesced cowl shocks was thus proposed and proven to significantly improve the inlet restart capability. (C) 2018 Elsevier Masson SAS. All rights reserved. |
分类号 | 一类 |
URL标识 | 查看原文 |
WOS关键词 | PERFORMANCE |
WOS研究方向 | Engineering, Aerospace |
语种 | 英语 |
WOS记录号 | WOS:000426332900008 |
资助机构 | Hong Kong Polytechnic University Central Research Grants [G-UA2M, G-YBGA] ; "Open Fund" of State Key Laboratory of High-Temperature Gas Dynamics, Chinese Academy of Sciences ; National Natural Science Foundation of China [11472279, 11672309] |
源URL | [http://dspace.imech.ac.cn/handle/311007/77922] ![]() |
专题 | 力学研究所_高温气体动力学国家重点实验室 空天飞行科技创新研究中心(筹) |
作者单位 | 1.Chinese Acad Sci, Inst Mech, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China 2.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China 3.Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong, Hong Kong, Peoples R China |
推荐引用方式 GB/T 7714 | Yue LJ,Jia YN,Xu X,et al. Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2018,74:72-80. |
APA | 岳连捷,贾轶南,Xu X,张新宇,&张鹏.(2018).Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers.AEROSPACE SCIENCE AND TECHNOLOGY,74,72-80. |
MLA | 岳连捷,et al."Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers".AEROSPACE SCIENCE AND TECHNOLOGY 74(2018):72-80. |
入库方式: OAI收割
来源:力学研究所
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