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Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
Authors:  Xue, Rui;  Zheng, Xing;  Yue LJ(岳连捷);  Zhang, Qian;  He, Xin;  Yang, Jing;  Weng, Chao;  Li, Zhihao
Adobe PDF(5483Kb)  |  Favorite  |  View/Download：156/48  |  Submit date：2022/10/25
Boundary layer combustion  Skin-friction reduction  Supersonic combustion  Scramjet engine  
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)
Adobe PDF(2818Kb)  |  Favorite  |  View/Download：313/119  |  Submit date：2021/01/29
Shock-shock interaction  Machine learning  Hypersonic flow  Impinging jet  Genetic programming  Triple point  
Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 92, 页码: 676-684
Authors:  Fang YS(方宜申);  Zhang ZJ(张子健);  Hu ZM(胡宗民);  Deng, X
View  |  Adobe PDF(2321Kb)  |  Favorite  |  View/Download：354/87  |  Submit date：2019/10/21
Oblique detonation wave  Blunt wedge  Initiation  Hydrogen