Results indicated that gust load on sweptback wing airplanes was dependent on lift curve slope of equivalent straight wing multiplied by cosine of angle of sweep and on effect of gradual penetration of gust on unsteady lift function.


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    Title :

    Tests of 45° sweptback-wing model in Langley gust tunnel


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    25 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :