Abstract A new approach to solving the task of stability for a circular cylindrical shell under axial compression is presented, taking into account the dynamic buckling. The modification of the algorithm for solving the known problem by the Ritz method is also proposed that allows investigating the effect of geometrical factors on the buckling load.
Stability of a cylindrical shell under axial compression
Russian Aeronautics (Iz VUZ) ; 58 , 1 ; 106-111
2015-01-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Stability of a cylindrical shell under axial compression
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