Results indicate that loading over ailerons was established by wing flow characteristics, and loading shapes were irregular in transonic speed range; other findings.


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    Title :

    Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on 4-percent-thick sweptback-wing-body model and pressure-distribution measurements on inboard aileron


    Additional title:

    NASA -- Tech Note


    Contributors:
    Runckel, J.F. (author) / Hieser, G. (author)


    Publication date :

    1961


    Size :

    55 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :