Wole Oyeyele
Member
Hi, I have a flying wing with a 25 degree wing sweep, and 0.7m of wing span. The wing loading is about 4.1Kg/m^2. The weight is about 320g. It has a flat bottom airfoil and no pitch (the bottom of the wing is exactly parallel to the direction of travel).
Is it possible to calculate the stall speed or minimum take off speed based on that information? I do not need a super accurate result, just a rough estimate will do.
Is it possible to calculate the stall speed or minimum take off speed based on that information? I do not need a super accurate result, just a rough estimate will do.