Stanford data of the wing's lifting force:
http://adg.stanford.edu/aa241/highlift/clmaxest.html
Lift Coefficient: http://en.wikipedia.org/wiki/Lift_coefficient
How to get most of the wing..what foil to choose...what needs to be considered ?
Needed formulas to calculate the lift:
http://www.ajdesigner.com/phpwinglift/wing_lift_equation_force.php
I like this last one alot !
I got take off speed clean 136 km/h
Flaps 15 Deg 89 km/h
Stall 62 km/h
Approximations only for MAX III ! I think 3-3.4 m2 wing is the right size.
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