The thickness ratio appeared to have little effect on lift coefficient at zero angle of attack, since the angle of zero lift was largely determined by the airfoil camber.

 
  • 在迎角為零時(shí),由于零升力主要由機翼中弧線(xiàn)決定,相對厚度對升力幾乎沒(méi)有影響。
今日熱詞
目錄 附錄 查詞歷史
国内精品美女A∨在线播放xuan