The damping process of the intensity of the influence of wingtip vortex on a following airplane is presented on the base of the measured circumferential velocity profile.
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美
释义
利用激光测速仪在水洞中测量了有无扰流片时翼梢涡的周向速度分布,给出了翼梢涡影响标度的衰减曲线。
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