An extension is made to the theory on which most aircraft pressure cabins are designed. In the existing theory the effect of the curvature of the deformed cylinder is neglected. This paper examines the manner in which this effect influences the stress distribution.


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    Title :

    Pressure Cabin Analysis


    Subtitle :

    An Extension to Existing Theory


    Contributors:

    Published in:

    Publication date :

    1960-05-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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