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Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
Authors:  Jiang ZL(姜宗林);  Teng, Honghui
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激波风洞高低压段钢膜片破裂特性研究 期刊论文
力学学报, 2021, 卷号: 53, 期号: 06, 页码: 1747-1757
Authors:  聂少军;  汪运鹏;  薛晓鹏;  姜宗林
Adobe PDF(7665Kb)  |  Favorite  |  View/Download：277/75  |  Submit date：2021/11/12
激波风洞  主膜片  爆轰驱动  破裂特性  数值模拟  
Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
Authors:  Ma KF(马凯夫);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Scramjet engines  Shock-induced combustion ramjet engines  Supersonic combustion  Chapman-Jouguet detonation  
Effects of Different Particle Size Distributions on Aluminum Particle-Air Detonation 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 7, 页码: 3115-3128
Authors:  Zhang ZJ(张子健);  Wen CY;  Liu YF(刘云峰);  Zhang DL(张德良);  Jiang ZL(姜宗林)
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A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors:  Peng J(彭俊);  Zhang ZJ(张子健);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
Adobe PDF(2165Kb)  |  Favorite  |  View/Download：424/99  |  Submit date：2019/09/09
Shock reflection  Vibration excitation  Mach reflection  Transition criterion  Hypersonic flow  
Shock/shock interactions between bodies and wings 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
Adobe PDF(1161Kb)  |  Favorite  |  View/Download：328/79  |  Submit date：2018/10/30
Body And Wing  Flow Field  Hypersonic Flow  Shock/shock Interaction  Wave Configurations  
Block building programming for symbolic regression 期刊论文
NEUROCOMPUTING, 2018, 卷号: 275, 页码: 1973-1980
Authors:  Chen C;  Luo ZT(罗长童);  Jiang ZL(姜宗林)
View  |  Adobe PDF(676Kb)  |  Favorite  |  View/Download：413/137  |  Submit date：2018/02/08
Symbolic Regression  Separable Function  Block Building Programming  Genetic Programming  
振动激发对高超声速气动力/热影响 期刊论文
力学学报, 2017, 卷号: 49, 期号: 03, 页码: 616-626
Authors:  张子健;  刘云峰;  姜宗林
View  |  Adobe PDF(711Kb)  |  Favorite  |  View/Download：411/87  |  Submit date：2017/12/22
振动激发  气动力/热  边界层  高温气体效应  
高超声速下三维侧压进气道激波干扰的研究 会议论文
中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议, 中国陕西西安, 2016-08-17
Authors:  项高翔;  王春;  姜宗林
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高超声速流动  体-翼激波干扰  波系结构  流场区域  
Theoretical solutions to three-dimensional asymmetrical shock/shock interaction 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 8, 页码: 1208-1216
Authors:  Xiang GX(项高翔);  Wang C(王春);  Hu ZM(胡宗民);  Li XD;  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
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3d Asymmetrical Shock/shock Interaction  Spatial-dimension Reduction  Mach Reflection  Flow Field  Theoretical Analysis