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- W1970866724 abstract "The problems of thermal deformation and buckling of cylindrical shells arise in connection with air-frame bodies subjected to the aerodynamic heating at supersonic speeds and with combustion chambers and exhaust pipes exposed to extremely hot gases.The authors analyzed previously the thermal deformations of flat plates and pointed out that it was impossible to disregard the effect of temperature gradient dhrough the thickness on their deformations according to the temperature distribution and the boundary conditions.In this paper, the deformation and buckling of cylindrical shells subjected to heating are analyzed. Taking the finite deformation into account, the fundamental non-linear simultaneous partial differential equations for the thermoelastic problems of a cylindrical shell, including also the terms concerning the normal pressure as well as the effect of temperature gradient through the thickness, are derived from the variational principle and are analyzed for the following three extreme cases, that is, for the cases where1) the cylindrical shell, subjected to heating and normal pressure, is free from the constraints upon the thermal expansion and the axial displacement, but restrained laterally against the pressure at the edges, 2) the cylindrical shell is unrestrained longitudinally but fully restrained Iaterally at the edges, and3) the cylindrical shell is clamped completely at the edges, and then some discussions on the analytical and numerical results are given." @default.
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- W1970866724 date "1962-01-01" @default.
- W1970866724 modified "2023-10-18" @default.
- W1970866724 title "Deformation and Buckling of Cylindrical Shells Subjected to Heating" @default.
- W1970866724 doi "https://doi.org/10.2322/jjsass1953.10.105" @default.
- W1970866724 hasPublicationYear "1962" @default.
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