L = Lift 升力
CL = Co-efficient of Lift 升力系数
1/2 p = half rho (rho relates to air density) ½空气密度
V² = velocity squared (velocity is a vector quantity made up of speed and direction) 速度的平方
s = surface area of the wing 机翼表面积
匿名回答于2019-01-30 01:47:42
