副翼反操纵指在高速情况下,使用外侧副翼时,翼尖刚度不够大,导致的翼尖变形,从而使得迎角改变,气动力改变,使变形的那边的升力减小,以至于小于另一边升力,最终导致飞机横滚方向与期待相反的状况叫做副翼反操作现象。

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