Investigation included determination of rolling and yawing characteristics of airplane in abrupt aileron rolls with slotted flap at various settings ranging from 0° to 40°; effectiveness of ailerons greatly reduced at flap deflections greater than 20°.


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    Title :

    Flight measurements of lateral control characteristics of narrow-chord ailerons on trailing edge of full-span slotted flap


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    6 pages


    Remarks:

    13 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English