8 High Lift Systems and Maximum Lift Coefficients
8 - 2 Trailing edge high lift systems The plain flap (Fig. 8.1) is simply a pivoted rear section of an airfoil. Typically the flap depth cF amounts to 30% of the chord. The plain flap increases lift by increasing the airfoil camber. Ailerons, elevators and rudders are plain flaps.
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