relationship of ground effect and wing chord
Can any one direct me to or furnish info on the relationship between plane size (chord) and when that chord starts interacting with the ground surface.
Is their a factor that can be used to calculate when GE comes into play? If there is a relationship is it the same for landing and takeoff?
It seems that with a greater distance between the two it would lessen the landing 'float' of some models if the landing gear were 'taller'.
Thanks for the assist.
mikenlapaz