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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?

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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?

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  • $\begingroup$ Yeah that's perfect thank you! $\endgroup$
    – Evan
    Mar 29, 2021 at 22:29

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