General formula for strength of any flat sheet stiffener combination presented, necessary empirical constants being given for limited range of extruded stiffener shapes.


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    Title :

    Empirical formulas for allowable compression loads in stiffened sheet panels


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Reff, E.R. (author)


    Publication date :

    1939


    Size :

    6 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :