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Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing 期刊论文
Journal of Aircraft, 2009, 卷号: 46, 期号: 4, 页码: 1444-1450
Authors:  Yang GW(杨国伟);  Chen DW(陈大伟);  Cui K(崔凯);  Yang GW
Adobe PDF(1016Kb)  |  Favorite  |  View/Download:873/193  |  Submit date:2009/08/03
Navier-stokes Solver  Aircraft