METHOD for the stress analysis of the circular conical fuselage with flexible frames, subjected to a fairly general type of load distribution, was recently developed by the present writer in a paper published in the Journal of the Royal Aeronautical Society. This paper did not, however, make any attempt to deal with the question of cut-outs, and for the reason given below it later transpired that certain modifications of the basic theory were required before this problem could be solved.


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    Title :

    Matrix Analysis of the Circular Conical Fuselage


    Subtitle :

    A Development and Revision of an Earlier Paper to Include the case of Cut-outs


    Contributors:


    Publication date :

    1957-01-01


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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