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Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
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High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247
Authors:  Peng J(彭俊);  Luo ZT(罗长童);  Han ZJ(韩子健);  Hu ZM(胡宗民);  Han GL(韩桂来);  Jiang ZL(姜宗林)
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Shock-shock interaction  Machine learning  Hypersonic flow  Impinging jet  Genetic programming  Triple point  
On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
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hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
超高速流动模拟及热化学反应模型对比研究 期刊论文
北京航空航天大学学报, 2017, 卷号: 43, 期号: 06, 页码: 1173-1181
Authors:  周凯;  李旭东;  胡宗民;  姜宗林
View  |  Adobe PDF(652Kb)  |  Favorite  |  View/Download：417/89  |  Submit date：2017/12/22
超高速  膨胀管  数值模拟  热化学反应模型  适用范围  
Starting Process in a Large-Scale Shock Tunnel 期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
Authors:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
View  |  Adobe PDF(764Kb)  |  Favorite  |  View/Download：370/103  |  Submit date：2017/09/19
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.
View  |  Adobe PDF(995Kb)  |  Favorite  |  View/Download：528/135  |  Submit date：2016/12/08
3d Asymmetrical Shock/shock Interaction  Spatial-dimension Reduction  Mach Reflection  Flow Field  Theoretical Analysis  
Development of the detonation-driven expansion tube for orbital speed experiments 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700
Authors:  Jiang ZL(姜宗林);  Wu B(吴波);  Gao YL;  Zhao W(赵伟);  Hu ZM(胡宗民);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow  
On the numerical technique for the simulation of hypervelocity test flows 期刊论文
Computers & Fluids, 2015, 卷号: 106, 页码: 12-18
Authors:  Hu ZM(胡宗民);  Wang C(王春);  Jiang ZL(姜宗林);  Khoo BC;  Hu ZM(胡宗民)
View  |  Adobe PDF(1617Kb)  |  Favorite  |  View/Download：1623/936  |  Submit date：2014/11/27
Hypervelocity Test Flow  Dcd Scheme  Flux-splitting  Spurious Oscillation