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Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)最新文献

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A Modified Rotated HLLC Scheme with improved Convergence for Steady-state simulations 稳态模拟中一种改进的旋转HLLC格式
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019) Pub Date : 2019-07-17 DOI: 10.3850/978-981-11-2730-4_0121-CD
B. Zang, S VevekU, T. New, M. Azarpeyvand
{"title":"A Modified Rotated HLLC Scheme with improved Convergence for Steady-state simulations","authors":"B. Zang, S VevekU, T. New, M. Azarpeyvand","doi":"10.3850/978-981-11-2730-4_0121-CD","DOIUrl":"https://doi.org/10.3850/978-981-11-2730-4_0121-CD","url":null,"abstract":"","PeriodicalId":159720,"journal":{"name":"Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)","volume":"15 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-07-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125383596","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Numerical Investigation on Axisymmetric and Planar Shock Reflections in Steady Viscous Flow 定常粘性流动中轴对称与平面激波反射的数值研究
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019) Pub Date : 2019-07-01 DOI: 10.3850/978-981-11-2730-4_0334-cd
G. Shoev, H. Ogawa
{"title":"Numerical Investigation on Axisymmetric and Planar Shock Reflections in Steady Viscous Flow","authors":"G. Shoev, H. Ogawa","doi":"10.3850/978-981-11-2730-4_0334-cd","DOIUrl":"https://doi.org/10.3850/978-981-11-2730-4_0334-cd","url":null,"abstract":"","PeriodicalId":159720,"journal":{"name":"Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)","volume":"43 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116783051","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Hypersonic Flow Field-radiation Coupling for Saturn entry 土星入口的高超声速流场辐射耦合
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019) Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0332-cd
C. Jacobs, R. Gollan, P. Marriotto, P. Jacobs
{"title":"Hypersonic Flow Field-radiation Coupling for Saturn entry","authors":"C. Jacobs, R. Gollan, P. Marriotto, P. Jacobs","doi":"10.3850/978-981-11-2730-4_0332-cd","DOIUrl":"https://doi.org/10.3850/978-981-11-2730-4_0332-cd","url":null,"abstract":"","PeriodicalId":159720,"journal":{"name":"Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)","volume":"29 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125213939","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
A Numerical Study of Shock Wave Propagation in a Double Bent Duct at Various Angles 激波在不同角度双弯管道内传播的数值研究
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019) Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0063-cd
D. Igra, O. Igra
{"title":"A Numerical Study of Shock Wave Propagation in a Double Bent Duct at Various Angles","authors":"D. Igra, O. Igra","doi":"10.3850/978-981-11-2730-4_0063-cd","DOIUrl":"https://doi.org/10.3850/978-981-11-2730-4_0063-cd","url":null,"abstract":"","PeriodicalId":159720,"journal":{"name":"Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)","volume":"74 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127132226","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Characteristics of Turbulent Spots in a Hypersonic Transitional Boundary Layer Inferred from Dense Arrays of Thin-film Heat Transfer Gauges 由薄膜传热计密集阵列推断的高超声速过渡边界层湍流斑特征
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019) Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0359-cd
S. Raghunath, B. Khoo, D. Mee
{"title":"Characteristics of Turbulent Spots in a Hypersonic Transitional Boundary Layer Inferred from Dense Arrays of Thin-film Heat Transfer Gauges","authors":"S. Raghunath, B. Khoo, D. Mee","doi":"10.3850/978-981-11-2730-4_0359-cd","DOIUrl":"https://doi.org/10.3850/978-981-11-2730-4_0359-cd","url":null,"abstract":"","PeriodicalId":159720,"journal":{"name":"Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)","volume":"28 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125862784","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 2
Self-ignition Induced by an Imploding Arc-shaped Shock wave 内爆弧形激波引起的自燃
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019) Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0174-cd
Hou Zihao, Zhu Yujian, Li Zhufei, Y. Jiming, Yang Jianting
{"title":"Self-ignition Induced by an Imploding Arc-shaped Shock wave","authors":"Hou Zihao, Zhu Yujian, Li Zhufei, Y. Jiming, Yang Jianting","doi":"10.3850/978-981-11-2730-4_0174-cd","DOIUrl":"https://doi.org/10.3850/978-981-11-2730-4_0174-cd","url":null,"abstract":"","PeriodicalId":159720,"journal":{"name":"Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)","volume":"88 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126024783","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Transition in Hypersonic Wall-Bounded Flows 高超声速壁面流动中的转捩
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019) Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_cunbiao-cd
Yiding Zhu, Cunbiao Lee
{"title":"Transition in Hypersonic Wall-Bounded Flows","authors":"Yiding Zhu, Cunbiao Lee","doi":"10.3850/978-981-11-2730-4_cunbiao-cd","DOIUrl":"https://doi.org/10.3850/978-981-11-2730-4_cunbiao-cd","url":null,"abstract":"The hypersonic boundary-layer transition is a strategic focus in the fluid mechanics community. This article reviews recent developments in the study of the hypersonic boundary-layer transition, especially at Peking University. The hypersonic quiet wind tunnel is introduced as a necessary device to obtain real flight data in near space. The most important issues in the recent development of the transition in the hypersonic boundary layer are addressed. The instability, its contribution to the aerodynamic heating and artificial control are discussed.","PeriodicalId":159720,"journal":{"name":"Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)","volume":"24 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123597938","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Hypersonic Shock Impingement on a Heated Surface in the T4 Free-Piston Driven Shock Tunnel T4自由活塞驱动激波通道中受热表面的高超声速激波冲击
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019) Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0164-cd
E. W. K. Chang, W. Chan, T. Mcintyre, A. Veeraragavan
{"title":"Hypersonic Shock Impingement on a Heated Surface in the T4 Free-Piston Driven Shock Tunnel","authors":"E. W. K. Chang, W. Chan, T. Mcintyre, A. Veeraragavan","doi":"10.3850/978-981-11-2730-4_0164-cd","DOIUrl":"https://doi.org/10.3850/978-981-11-2730-4_0164-cd","url":null,"abstract":"Shock impingement is one of the fundamental shock/boundary layer interaction cases in hypersonic flight vehicles. The adverse pressure gradient due to an oblique shock significantly increases the pressure and thermal loads on the vehicle surface. In addition to the shock impingement, the effect of the heated surface temperature in realistic hypersonic flows has not been extensively investigated. This paper presents a numerical approach to investigate hypersonic shock impingement on heated walls. The numerical results showed that the extent of flow separation was increased by the elevated wall temperature. Following this numerical work, a flat-plate/shock generator model that has been designed will be experimentally tested at The University of Queenland’s T4 free-piston driven shock tunnel to compare the flow-field and the incipient separation predicted from twodimensional numerical simulations.","PeriodicalId":159720,"journal":{"name":"Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)","volume":"36 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123787988","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 1
Effect of Boundary Layer Suction on Shock Train Oscillations in an Inlet/Isolator Model 入口/隔振器模型中边界层吸力对激波串振荡的影响
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019) Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0155-cd
B. Nie, Li Zhufei, Rong Huang, Y. Jiming
{"title":"Effect of Boundary Layer Suction on Shock Train Oscillations in an Inlet/Isolator Model","authors":"B. Nie, Li Zhufei, Rong Huang, Y. Jiming","doi":"10.3850/978-981-11-2730-4_0155-cd","DOIUrl":"https://doi.org/10.3850/978-981-11-2730-4_0155-cd","url":null,"abstract":"","PeriodicalId":159720,"journal":{"name":"Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)","volume":"55 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123019749","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Thermal Response Simulation of Low Density Heat Shields Under An Arcjet Flow Condition 弧流条件下低密度隔热板热响应模拟
Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019) Pub Date : 1900-01-01 DOI: 10.3850/978-981-11-2730-4_0449-cd
T. Sakai, B. Owiti, Y. Ishida, H. Tanno
{"title":"Thermal Response Simulation of Low Density Heat Shields Under An Arcjet Flow Condition","authors":"T. Sakai, B. Owiti, Y. Ishida, H. Tanno","doi":"10.3850/978-981-11-2730-4_0449-cd","DOIUrl":"https://doi.org/10.3850/978-981-11-2730-4_0449-cd","url":null,"abstract":"","PeriodicalId":159720,"journal":{"name":"Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019)","volume":"18 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114143453","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
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