对带振荡的快速上仰翼型的非定常分离流问题进行了计算研究。
The problem of unsteady separated flow of rapidly pitching airfoil with oscillating motion is computationally studied.
结果表明：机翼快速上仰时，随上仰速率增大最大升力系数增高，即动态升力效应更明显；
The experimental results show that the maximum lift coefficient Cy max and stall incidence are increased with increased pitch up rate, when the wing is rapidly pitching up.
上仰机械装置保证了风机在高风速下也能运转，并且会在不损坏电子或机械部件的情况下产生两倍于额定功率的电量。
The upward furling mechanism ensures the Lakota will not "Hide" from high winds but continue to put out up to two times its rated power without damage to its electrical or mechanical components.
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