New approach to calculation of bending strength of semi-monocoque (and possibly fully monocoque) fuselage shells; method uses directly load deflection graphs obtained from laboratory compression tests on panels representative of shell at section under consideration, and is analogous to calculation of form factor for solid beam section.


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    Title :

    Bending of fuselage shells


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1949


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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