Originally Posted by Clandestino
You don't mind the summary being wrong as long as it's quick?
Absolutely yes, that's why I opened this thread. Because according to what I know (or let's say what I belive to know
) this is wrong.
It's not the only thing I think it's wrong. I saw also that best lift/drag ratio is obtained at Vmd which according to what I belive to know it's obtained at 1.32 Vmd for a jet, the tangent at the drag curve not the lower part, equal to best endurance...