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Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions
Peng J(彭俊); Li S(李帅); Yang F(杨帆); Lin MY(林明月); Han GL(韩桂来); Hu ZM(胡宗民)
Source PublicationCHINESE JOURNAL OF AERONAUTICS
2023-03
Volume36Issue:3Pages:96-106
ISSN1000-9361
AbstractThe interactions of oblique/bow shock waves are the key flow phenomena restricting the design and aerothermodynamic performance of high speed vehicles. Type III and Type IV Shock/ Shock Interactions(SSIs) have been extensively investigated, as such interactions can induce abnormal aerodynamic heating problems in hypersonic flows of vehicles. The transition process between these two distinct types of shock/shock interactions remains unclear. In the present study, a subclass of shock/shock interaction configuration is revealed and defined as Type IIIa. Type IIIa interaction can induce much more severe aerodynamic heating than a Type IV interaction which was ever reported to be the most serious in literature. The intense aerodynamic heating observed in this configuration highlights a new design point for the thermal protection system of hypersonic vehicles. A secondary Mach interaction between shock waves in the supersonic flow path of a Type III configuration is demonstrated to be the primary mechanism for such a subclass of shock/shock interaction configuration.(c) 2022 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY NC ND license (http://creativecommons.org/licenses/by nc nd/4.0/).
KeywordShock interactions Transitional configuration Aerodynamic heating Shear layer Mach interaction
DOI10.1016/j.cja.2022.08.006
Indexed BySCI ; EI ; CSCD
Language英语
WOS IDWOS:000951040000001
WOS Research AreaEngineering, Aerospace
WOS SubjectEngineering
Funding OrganizationNational Key Research and Development Plan of China [2019YFA0405204] ; National Natural Science Foundation of China [12172365, 12072353, 12132017]
Classification一类
Ranking1
ContributorLin, MY (corresponding author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China. ; Lin, MY (corresponding author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Cited Times:8[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/91849
Collection高温气体动力学国家重点实验室
Affiliation1.Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
2.Syst Design Inst Mech Elect Engn, Beijing 100854, Peoples R China
3.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China
Recommended Citation
GB/T 7714
Peng J,Li S,Yang F,et al. Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions[J]. CHINESE JOURNAL OF AERONAUTICS,2023,36,3,:96-106.Rp_Au:Lin, MY (corresponding author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China., Lin, MY (corresponding author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
APA 彭俊,李帅,杨帆,林明月,韩桂来,&胡宗民.(2023).Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions.CHINESE JOURNAL OF AERONAUTICS,36(3),96-106.
MLA 彭俊,et al."Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions".CHINESE JOURNAL OF AERONAUTICS 36.3(2023):96-106.
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