Abstract We present an algorithm for calculating the shells of revolution with the branching meridian using the triangular finite elements, the rigidity matrices of which are formed based on the vector method of displacement interpolation [1]. The correct kinematic and static conditions of shell conjugation on the line of their coupling have been developed. The shell structure consisting of a cylinder and adjacent shells is calculated under various conditions of support.
The finite element analysis of shells of revolution with a branching meridian
Russian Aeronautics (Iz VUZ) ; 52 , 1 ; 22-29
2009-03-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
The finite element analysis of shells of revolution with a branching meridian
Online Contents | 2009
|Finite element solution for thin shells of revolution
TIBKAT | 1964
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