Gareth Padfield's book Helicopter Flight Dynamics provides a method for calculating the reduction in induced flow velocity when in ground effect.
δV
i = A V
i / 16 π Z
g2
- δVi
- Difference In Induced Flow From OGE [m s-1]
- A
- Disc Area [m2]
- Vi
- Velocity of Induced Flow. [m s-1]
- Zg
- Height of Disc above the ground. [m]
Example Content