Investigation to study spin behavior of fighter type aircraft, carried out in Chance Vought low speed wind tunnel: exploratory one degree of freedom tests; 2-dimensional tests; determination of autorotation moments of complete model; it is revealed that fuselage nose, rather than wing, is major source of autorotative moment; other factors influencing spin behavior.


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    Title :

    Autorotation of fuselages


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1958


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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