Specifications concerning load assumptions and distribution adopted by German Institute for Aeronautical Research as basis of strength calculation.


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    Title :

    Load assumptions for calculating the strength of airplanes


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Memorandum



    Publication date :

    1930


    Size :

    31 pages


    Remarks:

    12 Figs., partly on supp. plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English






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