A study of thermal buckling of stiffened cylindrical shells with the proportions of a preliminary supersonic transport fuselage design (1970) is presented. The buckling analysis is performed using an axisymmetric shell-of-revolution code, BOSOR4. The effects of combined mechanical (axial loading) and thermal loading (heated skins) are investigated. Results indicate that the location of longitudinal eccentric stiffening has a very large effect on the thermal buckling strength of longitudinally stiffened shells, and on longitudinally stiffened shells with rings.


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    Title :

    Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells


    Additional title:

    Einfluß von Versteifung und mechanischer Beanspruchung auf das thermische Beulen von versteiften Zylinderschalen


    Contributors:
    Johnson, T.F. (author) / Card, M.F. (author)


    Publication date :

    1995


    Size :

    9 Seiten, 13 Bilder, 5 Tabellen, 6 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English






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