The effect of aspect ratio and angle of attack on wing-plate junction flow
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https://data.mendeley.com/datasets/b39sxdbtpx
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资源简介：
The mean pressure of the flow field formed within wing-body junctions are presented. Wings formed from constant-chord, NACA 0012 airfoil sections were used, with aspect ratios of 0.2 and 1.0 and angles of attack of 0, 5 and 10 degree.
创建时间：
2019-11-01
