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Force measurement using strain-gauge balance in shock tunnel based on deep learning 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 8, 页码: 43-53
Authors:  Nie SJ(聂少军);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2346Kb)  |  Favorite  |  View/Download：55/11  |  Submit date：2024/02/26
Convolutional neural net-works  Deep learning  Frequency domain analysis  Force measurement  Time domain analysis  Recurrent neural networks  
A theoretical method for solving shock relations coupled with chemical equilibrium and its applications 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 6, 页码: 47-62
Authors:  Zhang, Zijian;  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(3178Kb)  |  Favorite  |  View/Download：239/56  |  Submit date：2022/07/18
Chemical equilibrium  Detonation  Dissociated air  Shock relation  Theoretical solution  
Oblique detonation wave triggered by a double wedge in hypersonic flow 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184
Authors:  Teng, Honghui;  Zhang, Yuhang;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(1747Kb)  |  Favorite  |  View/Download：180/38  |  Submit date：2022/07/18
Double wedge  Hypersonic flow  Initiation structures  Oblique detonation  Shock interactions  
Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2554Kb)  |  Favorite  |  View/Download：152/33  |  Submit date：2022/06/10
Boundary layer correction  High-enthalpy flow  Hypersonic wind tunnel  Nozzle design  Real-gas effects  
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  Favorite  |  View/Download：286/58  |  Submit date：2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
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)
Adobe PDF(1129Kb)  |  Favorite  |  View/Download：337/173  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
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)
View  |  Adobe PDF(1161Kb)  |  Favorite  |  View/Download：314/75  |  Submit date：2018/10/30
Body And Wing  Flow Field  Hypersonic Flow  Shock/shock Interaction  Wave Configurations