Experiment results indicate that the flexible wing has a larger angle of stall and a greater maximum lift coefficient than the fixed wing.
对比结果表明:柔性翼相比于对应的刚性翼,失速迎角较大;
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.
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;
On this type of airfoil vortex generators (also called micro-vortex generators, or VGs) add very little improvement with respect to the maximum lift coefficient (or stall speed).
对这种类型的翼型涡发生器(也称为微型涡发生器,或vgs)添加很少的改善方面的最高升力系数(或失速速度)。
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