Leading edges of 24 ST Alclad, reinforced by conventional ribs, and chordwise or spanwise stiffeners; wide range of design parameters covered, including both newer and older wing types; comparison with findings of NACA -- Tech Note 2362.


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    Title :

    Empirical formula for ultimate shear strength of wing leading edges


    Additional title:

    Svenska Aeroplan Aktiebolaget -- Tech Note


    Contributors:
    Turner, F. (author)


    Publication date :

    1952


    Size :

    22 pages


    Remarks:

    Diagrams, Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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