Im building a v22 osprey that will have tilting rotors.The wing span is 65 inches chord 12 inches.Problem is transitioning from hover to forward flight with rotors at 60 degrees. The wing loading is 50 ounces per square foot. Further thought should be given to the fact that during low speed transition the rotors will impart significant down thrust. Was thinking of either a naca 23016 or a S8036. I need lots of lift and forgiving stall characteristics. Help!!!!