stanislavz
Well-Known Member
Just for better understanding. I do come to this question from this pdf : contrails.free.fr/temp/Pilot100Yrs-06-164.pdf
Smilar approach was done on Blanik ~ also on 40% of used chord. Books do suggest as general rule 20-25 %.
So the question is simple one. Taking same wing, with same area and same area of aileron, but first one is for example half span and 25% of chord (12.5% of total area), other one - 40% of chord, but 31.25 % of span..
Which one will be better, and at which points ?
Smilar approach was done on Blanik ~ also on 40% of used chord. Books do suggest as general rule 20-25 %.
So the question is simple one. Taking same wing, with same area and same area of aileron, but first one is for example half span and 25% of chord (12.5% of total area), other one - 40% of chord, but 31.25 % of span..
Which one will be better, and at which points ?