XFOIL Version 6.96 was used to produce aerodynamic characteristics of the GN-1 Aircamper airfoil at the quoted stall speed, i.e. 22 knots (25 mph). The Reynolds number equating to this free air velocity at sea level is approximately Re = 1,164,000.
It turns out that the maximum calculated lift coefficient at a free air velocity of 22 knots for the GN-1 Aircamper airfoil is Clmax = 1.45.
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