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Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
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Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:  Yao W(姚卫);  Liu H(刘杭);  Yue LJ(岳连捷);  Xiao YB(肖雅彬)
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Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
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
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Boundary layer combustion  Skin-friction reduction  Supersonic combustion  Scramjet engine  
Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 112, 页码: 9
Authors:  Wang KL(王宽亮);  Yang PF(杨鹏飞);  Teng HH(滕宏辉)
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Oblique detonation  Wave complex  Instability  Thermal choking  Expansion corner  
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
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Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors:  Zhang ZJ(张子健);  Ma KF(马凯夫);  Zhang WS(张文硕);  Han X(韩鑫);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Oblique detonation engine  Pre-injection  Detonative combustion  Mixing  Hydrogen  
Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
Authors:  Luo K(罗凯);  Wang Q(汪球);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
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Quasi-one-dimensional  Detonation  Shock tunnel  Shock speed  
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  
Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
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Hybrid rocket engine  Paraffin-based fuel  Acrylonitrile-butadiene-styrene  Regression rate  Combustion efficiency  
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
Authors:  Wang KL(王宽亮);  Li F(李飞);  Zou PF(邹鹏飞);  Lin X(林鑫);  Mao RH(毛荣海);  Yu XL(余西龙)
View  |  Adobe PDF(2678Kb)  |  Favorite  |  View/Download：276/62  |  Submit date：2020/03/21
Swirl flame  Heat release  Chemiluminescence  3D-CTC