Quote:
Originally Posted by aerohead
Did you get a satisfactory answer?
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What do you think? I think not. And suprise, there is a reason for the question if you are a fan of 12-25% thicknesses NACA airfoils of the laminar persuasion with the max thickness aft of of 40%
Has to do with boundary layers being undefined subsonic (low reynolds) but still creating a very low drag profile @ low speeds