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Separate and Combined Effects of Surface Roughness and Thermal Barrier Coating on Vane Cooling Performance 期刊论文
JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS, 2020, 卷号: 12, 期号: 5, 页码: 15
作者:  Prapamonthon P;  Yin B(银波);  Yang GW(杨国伟);  Zhang MH
Adobe PDF(2963Kb)  |  收藏  |  浏览/下载:294/103  |  提交时间:2020/11/30
gas-turbine heat transfer  surface roughness  cooling performance  thermal barrier coating  
Fixed-Point Fluid structure interaction analysis BASED ON geometrically exact approach 期刊论文
SCIENTIFIC REPORTS, 2020, 卷号: 10, 期号: 1, 页码: 16
作者:  Yu ML(余明亮);  Nie XY(聂雪媛);  Yang GW(杨国伟);  Zhong PN(钟培楠)
Adobe PDF(4371Kb)  |  收藏  |  浏览/下载:272/86  |  提交时间:2020/08/26
Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 171, 页码: 300-310
作者:  Ju SJ;  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3216Kb)  |  收藏  |  浏览/下载:308/82  |  提交时间:2020/05/18
Computational fluid dynamics  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
Time efficient aeroelastic simulations based on radial basis functions 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2017, 卷号: 330, 页码: 810-827
作者:  Liu W(刘文);  Huang CD(黄程德);  Yang GW(杨国伟);  Liu, W (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(5302Kb)  |  收藏  |  浏览/下载:357/104  |  提交时间:2017/04/26
Transonic Aeroelastic Numerical Simulation in Aeronautical Engineering 期刊论文
International Journal of Computational Fluid Dynamics,2006,20(5):339-347, 2006
作者:  Yang GW(杨国伟);  Yang, GW (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100080, Peoples R China.
Adobe PDF(2170Kb)  |  收藏  |  浏览/下载:434/111  |  提交时间:2007/06/15
Transonic Aeroelastic Numerical Simulation in Aeronautical Engineering 会议论文
13th Annual Conference of the CFD-Society-of-Canada, JUL 31-AUG 02, 2005 St Johns, CANADA
作者:  Yang GW(杨国伟)
Adobe PDF(2156Kb)  |  收藏  |  浏览/下载:445/114  |  提交时间:2007/12/18
Numerical Analyses of Transonic Fluid/Structure interaction in Aircraft Engineering 会议论文
Sixth World Congress on Computational Mechanics in Conjunction with the Second Asian-Pacific Congress on Computational Mechanics, Sept. 5-10, 2004, Beijing, China
作者:  Yang GW(杨国伟);  Obayashi S
Adobe PDF(1646Kb)  |  收藏  |  浏览/下载:851/241  |  提交时间:2007/12/18
Numerical Analyses of Discrete Gust Response for an Aircraft 期刊论文
Journal of Aircraft, 2004, 卷号: 41, 期号: 6, 页码: 1353-1359
作者:  Yang GW(杨国伟);  Obayashit S
Adobe PDF(102Kb)  |  收藏  |  浏览/下载:749/249  |  提交时间:2007/06/15
Numerical analyses of discrete gust response for a flexible aircraft 会议论文
21st AIAA Applied Aerodynamics Conference 2003, Orlando, FL, United states, June 23, 2003 - June 26, 2003
作者:  Yang GW(杨国伟);  Obayashi S
Adobe PDF(1991Kb)  |  收藏  |  浏览/下载:165/72  |  提交时间:2017/06/01
Direct-coupling Method  Dynamic Equations Of Motion  Flexible Aircraft  Flexible Airplane  Freedom Of Motion  One-minus-cosine Gust  Quasi-steady Model  Supersonic Transport