Experimental and theoretical evidence drawn upon to show that, due to shear lag, airplane wing with longitudinal stringers should be less efficient from strength weight standpoint than wing which does not have longitudinal stringers in addition to main wing beams.


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    Titel :

    Effect of shear lag upon wing strength


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Sibert, H.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1939


    Format / Umfang :

    3 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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