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RPM on a fixed pitched propeller

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Old 1st Oct 2009, 02:46
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If you want to score an A+, check out the negative AOA required on an an asymetrical wing, for a zero-lift part of flight.
Approx. -4 degrees for a light aircraft? Again, depending on the design of the wing. The reason why at 0 degrees AoA the wing is still producing lift is because the upper surface of the wing is still accelerating air, therefore decrease in static pressure and producing lift ?
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