Recent tests conducted in 7 by 10-ft wind tunnel of University of Detroit; slotted flap of 30% chord fitted on Goettingen 398 (modified) airfoil, showing large increase in lift with very small added drag for small flap deflections.


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    Title :

    Airfoil fitted with slotted flap


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Publication date :

    1936


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





    STALL HYSTERESIS OF AN AIRFOIL WITH SLOTTED FLAP

    Biber, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2005


    Stall Hysteresis of an Airfoil with Slotted Flap

    Biber, K. | Online Contents | 2005