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Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 18
作者:  Guo SQ(郭帅旗);  Liu W(刘文);  Zhang CA(张陈安);  Liu Y(刘洋);  Wang FM(王发民)
收藏  |  浏览/下载：25/0  |  提交时间：2024/02/05
Hypersonic waverider  Aerodynamic model  Symbolic regression  Bluntness effect  
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11
作者:  Liu, Mingjiang;  Sun, Mingbo;  Zhao, Guoyan;  Meng Y(孟宇);  Huang, Yuhui;  Ma, Guangwei;  Wang, Hongbo
Adobe PDF(3841Kb)  |  收藏  |  浏览/下载：104/24  |  提交时间：2022/12/20
Tandem-cavity  Scramjet combustor  Combustion mode  Thrust performance  
Three-dimensional flow structures and heat transfer characteristics of compressible flow over a cylindrical cavity 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 122, 页码: 12
作者:  Wang JT(王江涛);  Ma T(马特);  Wang Z(王哲);  Wang RX(王睿星);  Song HW(宋宏伟);  Yuan W(袁武);  Zheng HW(郑洪伟)
Adobe PDF(4247Kb)  |  收藏  |  浏览/下载：133/13  |  提交时间：2022/06/10
Cylindrical cavity  Heat transfer  Compressible flow  3D flow behaviors  
A numerical study of oblique detonation re-stabilization by expansion waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 122, 页码: 8
作者:  Yao KP(姚克鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(1789Kb)  |  收藏  |  浏览/下载：217/38  |  提交时间：2022/06/10
Oblique detonation  Stationary  Thermal choking  Expansion waves  
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
作者:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1961Kb)  |  收藏  |  浏览/下载：270/103  |  提交时间：2020/05/18
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
作者:  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)
浏览  |  Adobe PDF(2678Kb)  |  收藏  |  浏览/下载：270/61  |  提交时间：2020/03/21
Swirl flame  Heat release  Chemiluminescence  3D-CTC  
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
作者:  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)
Adobe PDF(2678Kb)  |  收藏  |  浏览/下载：206/68  |  提交时间：2020/03/21
Swirl flame  Heat release  Chemiluminescence  3D-CTC  
Numerical study on initiation of oblique detonations in hydrogen-air mixtures with various equivalence ratios 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 卷号: 49, 页码: 130-134
作者:  Zhang YN;  Gong JS;  Wang T(王涛);  Zhang, YN (reprint author), Beijing Power Machinery Res Inst, State Key Lab Laser Prop & Applicat, Beijing 100074, Peoples R China.
Adobe PDF(1388Kb)  |  收藏  |  浏览/下载：486/121  |  提交时间：2016/03/21
Detonation  Hydrogen  Initiation  Hypersonic  
Tunable diode laser absorption spectroscopy measurements of high-pressure ammonium dinitramide combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 45, 页码: 140-149
作者:  Yao, Zhaopu;  Zhang, Wei;  Wang, Meng;  Chen, Jun;  Shen, Yan;  Wei, Yanming;  Yu XL(余西龙);  Li F(李飞);  Ceng H(曾徽);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Unknown(1847Kb)  |  收藏  |  浏览/下载：240/69  |  提交时间：2015/10/21
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
作者:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1112Kb)  |  收藏  |  浏览/下载：544/226  |  提交时间：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas