Stress analysis of rear wing spar with trailing-edge flaps, using general method and nomenclature given in Airplane Structures, by NILES and NEWELL; equations for single span; maximum moment; equation of three moments.


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    Title :

    Precise moment equations


    Additional title:

    Aero Digest


    Contributors:

    Published in:

    Aero Digest ; 27 , n 6


    Publication date :

    1935


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :