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Wing profile for the Bf 108 "Typhoon"
We know that the wing profile for the Bf 109 was NACA 2R1, with a thickness of 14.2% at the wing roots, and 11% at the wingtips. But , does anyone know the comparable values for the Bf 108, since apparently, Prof. Messerschmitt wanted to use its wing shape for the Bf 109.
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