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Dynamic Impact of High-Density Aluminum Foam 期刊论文
ACTA MECHANICA SOLIDA SINICA, 2022, 卷号: 35, 期号: 2, 页码: 198-214
作者:  Peng Q(彭青);  Xie JJ(谢季佳);  Ma HS(马寒松);  Ling, X;  Liu XM(刘小明);  Wei YG(魏悦广)
Adobe PDF(2146Kb)  |  收藏  |  浏览/下载：353/117  |  提交时间：2021/08/30
High density aluminum  Foam Deshpande-Fleck model  Finite element method  Impact analysis  Plastic wave  
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
作者:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2554Kb)  |  收藏  |  浏览/下载：143/28  |  提交时间：2022/06/10
Boundary layer correction  High-enthalpy flow  Hypersonic wind tunnel  Nozzle design  Real-gas effects  
Multi-parameter joint optimization for double-strip high-speed pantographs to improve pantograph-catenary interaction quality 期刊论文
ACTA MECHANICA SINICA, 2022, 卷号: 38, 期号: 1, 页码: 11
作者:  Wu MZ(吴孟臻);  Xu XH(许向红);  Yan YZ(燕永钊);  Luo Y(罗弈);  Huang, Sijun;  Wang, Jianshan
Adobe PDF(2796Kb)  |  收藏  |  浏览/下载：169/45  |  提交时间：2022/07/18
High-speed pantograph  Pantograph-catenary interaction quality  Multi-parameter joint optimization  
Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
作者:  Chen KT(陈科挺);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(511Kb)  |  收藏  |  浏览/下载：201/39  |  提交时间：2022/01/12
Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency  
Experimental and numerical investigations into flow features in an intake duct for the waterjet propulsion under mooring conditions 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 18
作者:  Huang RF(黄仁芳);  Zhang, Ruizhi;  Wang YW(王一伟);  Luo, Xianwu;  Zhu, Lei
Adobe PDF(11187Kb)  |  收藏  |  浏览/下载：225/44  |  提交时间：2021/06/21
Waterjet propulsion  Particle image velocimetry (PIV)  Intake duct  Waterjet pump  Mooring conditions  
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
作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  收藏  |  浏览/下载：322/169  |  提交时间：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
作者:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
Adobe PDF(1090Kb)  |  收藏  |  浏览/下载：252/101  |  提交时间：2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
Experimental investigation of a hypersonic I-shaped configuration with a waverider compression surface 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2020, 卷号: 63, 期号: 5, 页码: 3
作者:  Li GL(李广利);  Cui K(崔凯);  Xu YZ(徐应洲);  Wang HX(王浩祥);  Yang J(杨靖);  Xu XG(许先贵)
Adobe PDF(661Kb)  |  收藏  |  浏览/下载：367/87  |  提交时间：2020/05/18
A nonlinear model for aerodynamic configuration of wake behind horizontal-axis wind turbine 期刊论文
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2019, 卷号: 40, 期号: 9, 页码: 1313-1326
作者:  Li DS;  Guo T;  Li RN;  Yang CX;  Cheng ZX;  Li Y;  Hu WR(胡文瑞)
Adobe PDF(1504Kb)  |  收藏  |  浏览/下载：171/73  |  提交时间：2019/10/21
nonlinear wake aerodynamic model  vortex-induced velocity  integral equation of vortex-induced velocity  horizontal-axis wind turbine  O355