Problems in designing plane around given engine with minimum of deadweight and maximum of useful load, at same time fulfilling demands for strength of all structural and control parts; tables give data on weights of items of all structural parts on which designer has direct influence; and their percentage of weight empty for Fokker Super-Universal, F-10-A, and F-32.


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    Title :

    The airplane weight complex


    Additional title:

    Aviation


    Contributors:

    Published in:

    Aviation ; 29 , n 4


    Publication date :

    1930


    Size :

    6 pages


    Remarks:

    4 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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