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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
Authors:  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.
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Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes 会议论文
54th AIAA Aerospace Sciences Meeting, 2016, San Diego, CA, United states, January 4, 2016 - January 8, 2016
Authors:  Gan JY;  Shen YQ(申义庆);  Zha GC
View  |  Adobe PDF(555Kb)  |  Favorite  |  View/Download：317/101  |  Submit date：2017/05/05
Central Differencing  Drag Prediction  Finite Difference Scheme  High  Order Scheme  Line Relaxation  Mesh Refinement  Trailing Edges  Turbulent Models  
Fast Dynamic Mesh Method and its Application on Aeroelasticity 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:  Yang GW(杨国伟);  Zheng GN(郑冠男);  Nie XY(聂雪媛)
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Dynamic Mesh  Rbf  Reduced-point Option  Aeroelasticity  
The Effect of Conical Flowfields on the Performance of Waveriders at Mach 6 期刊论文
Chinese Science Bulletin, 2007, 卷号: 52, 期号: 1, 页码: 57-64
Authors:  Cui K(崔凯);  Yang GW(杨国伟);  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100080, Peoples R China.
Adobe PDF(655Kb)  |  Favorite  |  View/Download：754/259  |  Submit date：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
Authors:  Yang GW(杨国伟);  Obayashi S
View  |  Adobe PDF(1991Kb)  |  Favorite  |  View/Download：210/87  |  Submit date：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