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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  
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH(马生虎);  Zhang QF(张启帆);  Zhang, Peng;  Zhang XY(张新宇)
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Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
Space-Time Conservation Element and Solution Element Method and Its Applications 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 12, 页码: 5408-5430
Authors:  Jiang YZ;  Wen CY;  Zhang DL(张德良)
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A Data-Correlation Model of Aerodynamic Heating Based on Globally Optimal Learning Method 会议论文
16th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery (ICNC-FSKD 2020), 西安,中国, 19-21 December 2020
Authors:  Chen Z(陈阵);  Li S(李森);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
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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  
Numerical investigation of flow structures resulting from the interaction between an oblique detonation wave and an upper expansion corner 期刊论文
JOURNAL OF FLUID MECHANICS, 2020, 卷号: 903, 页码: 17
Authors:  Wang KL(王宽亮);  Teng HH(滕宏辉);  Yang PF(杨鹏飞);  Ng HD
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detonation waves  
Intelligent Force-Measurement System Use in Shock Tunnel 期刊论文
SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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artificial intelligence  BALANCE SYSTEM  deep learning  DESIGN  dynamic calibration  FLOWS  force-measurement system  strain-gauge balance  
Unsteady combustion mode with a super-high frequency induced by a curved shock 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 11, 页码: 116101
Authors:  Teng HH(滕宏辉);  Liu S;  Zhang ZJ(张子健)
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PROJECTILE  MECHANISM  SYSTEMS  
Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Shock tunnel  High enthalpy  Aerodynamic force measurement  Strain gauge balance  
Cellular Aluminum Particle-Air Detonation Based on Realistic Heat Capacity Model 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2020, 卷号: 192, 期号: 10, 页码: 1931-1945
Authors:  Xiang GX(项高翔);  Yang PF(杨鹏飞);  Teng HH(滕宏辉);  Jiang ZL(姜宗林)
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Al particle  cellular detonation  heat capacity  hybrid model