New mechanics solutions for Bodenplatte aircrafts.

[KatieLuna]

On 6/5/2018 at 3:36 PM, AeroAce said:

Btw modelling a normal wing is technically harder than a laminar wing from an aerodynamics point of view because in theory you don't have to model turbulence for a laminar wing. Turbulence modeling is one of the hardest things to calculate. 

I'm fairly certain that a laminar flow wing  does not keep the flow laminar across the whole chord, and instead trys to keep it laminar for as long as possible (typically 60%-ish of the chord, as opposed to perhaps 20% on standard foil sections).