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Shock/shock interactions between bodies and wings
Xiang GX(项高翔); Wang C(王春); Teng HH(腾宏辉); Jiang ZL(姜宗林)
2018-02-01
发表期刊CHINESE JOURNAL OF AERONAUTICS
卷号31期号:2页码:255-261
ISSN1000-9361
摘要

This paper examines the Shock/Shock Interactions (SSI) between the body and wing of aircraft in supersonic flows. The body is simplified to a flat wedge and the wing is assumed to be a sharp wing. The theoretical spatial dimension reduction method, which transforms the 3D problem into a 2D one, is used to analyze the SSI between the body and wing. The temperature and pressure behind the Mach stem induced by the wing and body are obtained, and the wave configurations in the corner are determined. Numerical validations are conducted by solving the inviscid Euler equations in 3D with a Non-oscillatory and Non-free-parameters Dissipative (NND) finite difference scheme. Good agreements between the theoretical and numerical results are obtained. Additionally, the effects of the wedge angle and sweep angle on wave configurations and flow field are considered numerically and theoretically. The influences of wedge angle are significant, whereas the effects of sweep angle on wave configurations are negligible. This paper provides useful information for the design and thermal protection of aircraft in supersonic and hypersonic flows. (C) 2018 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics.

关键词Body And Wing Flow Field Hypersonic Flow Shock/shock Interaction Wave Configurations
DOI10.1016/j.cja.2017.11.012
URL查看原文
收录类别SCI ; EI ; CSCD
语种英语
WOS记录号WOS:000427445000006
关键词[WOS]Planar Shock ; Flows
WOS研究方向Engineering, Aerospace
WOS类目Engineering
项目资助者Fundamental Research Funds for the Central Universities of China [31020170QD087]
论文分区二类/q1
力学所作者排名1
引用统计
文献类型期刊论文
条目标识符http://dspace.imech.ac.cn/handle/311007/77880
专题高温气体动力学国家重点实验室
通讯作者Wang C(王春)
作者单位1.Northwestern Polytech Univ, Sch Mech Civil Engn & Architecture, Xian 710129, Shaanxi, Peoples R China
2.Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Xiang GX,Wang C,Teng HH,et al. Shock/shock interactions between bodies and wings[J]. CHINESE JOURNAL OF AERONAUTICS,2018,31(2):255-261.
APA Xiang GX,Wang C,Teng HH,&Jiang ZL.(2018).Shock/shock interactions between bodies and wings.CHINESE JOURNAL OF AERONAUTICS,31(2),255-261.
MLA Xiang GX,et al."Shock/shock interactions between bodies and wings".CHINESE JOURNAL OF AERONAUTICS 31.2(2018):255-261.
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