Maximum angular accelerations in roll and yaw produced by sudden application of ailerons and maximum accelerations in yaw produced by sudden application of rudder during gliding flight recorded for following wing arrangements: no auxiliary device; full-span slots; plain flaps; flaps and full-span slots.


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    Title :

    Effect of slots and flaps on lateral control of low-wing monoplane as determined in flight


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Soule, H.A. (author) / Wetmore, J.W. (author)


    Publication date :

    1933


    Size :

    11 pages


    Remarks:

    12 Supp Sheets


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English