What is the CLmax of the CF-100 Canuck? I've been struggling to find specifications for the CF-100 Canuck. What is the CLmax of the CF-100 Canuck and how can I find it?
The CF-100 had a symmetrical NACA 0010 airfoil, which had a Clmax of just under 1.4. according to Airfoil Tools.com (Xfoil).  Is that what you are looking for?