Experiment results indicate that the flexible wing has a larger angle of stall and a greater maximumliftcoefficient 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;
2
The experimental results show that the maximumliftcoefficient 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;
3
On this type of airfoil vortex generators (also called micro-vortex generators, or VGs) add very little improvement with respect to the maximumliftcoefficient (or stall speed).