204 research outputs found

    Estimation of possible increase in Cp by use of Winglets

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    ATEFlap Aerodynamic Model, a dynamic stall model including the effects of trailing edge flap deflection

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    Modelling the influence of yaw using a simple vortex rotor model

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    Thick Airfoils and High Lift

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    An improved tip-loss correction based on vortex code results

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