Abstract A technique for calculating the geometrically and physically nonlinear stress strain state of nonshallow shells of revolution under the nonaxisymmetric wind-like loading is proposed. The calculation results for a semispherical shell with the central hole and rigidly fixed edges depending on the loading nonaxisymmetry, material characteristics and thickness are presented. We demonstrate not only quantitative but also qualitative influence of taking into account the factor of joint nonlinearity on the process of shell deformation.
A technique for calculating large deflections of nonshallow elastoplastic shells of revolution under nonaxisymmetric loading
Russian Aeronautics (Iz VUZ) ; 50 , 4 ; 349-356
2007-12-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
General theory of large deflections of thin shells
TIBKAT | 1961
|Calculation of finite axisymmetric deflections of thin short shells of revolution
British Library Online Contents | 1996
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