I'm building an Experimental Champ, and I am thinking about using the NACA 23012 airfoil (used on Taylorcrafts). I have heard from the clipped wing Cubs folks that Taylorcraft wings have been sucessfully adapted to Cubs and Champs with good results. Does anyone have any information on this??
While I'm at it, does anyone know the following for a BC12-D: Wing area (183 sq. ft.), wing incidence angle with a/c level (looks like 2-1/2 degrees according to the rigging data and a layout of the airfoil), Horizontal stab area and incidence angle with the a/c level, Elevator area, Max take off weight, C.G. limits, Typical cruise speeds with a 65 hp engine.
Thanks
While I'm at it, does anyone know the following for a BC12-D: Wing area (183 sq. ft.), wing incidence angle with a/c level (looks like 2-1/2 degrees according to the rigging data and a layout of the airfoil), Horizontal stab area and incidence angle with the a/c level, Elevator area, Max take off weight, C.G. limits, Typical cruise speeds with a 65 hp engine.
Thanks
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