Various methods for determination of principal wing load factor for which data are available; results obtained by rational methods; new expression based on equations of motion and assuming instantaneous pull up from horizontal flight at maximum velocity; recommendations with regard to load factor to be assigned to airplanes both of restricted and unrestricted classes. From thesis submitted to Mass Inst Technology.


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    Title :

    Rationalization of load factors for aeroplane wings


    Additional title:

    Eng J


    Contributors:

    Published in:

    Publication date :

    1934


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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