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- W206027655 abstract "A computational efficiency method is presented to study the structure of a rocket fuel tank subjected to an internal pressure. The complete structure is divided into a number of substructures that can be analyzed separately by the displacement method. Finally, using the simultaneous relaxation of the substructures boundary, we find the actual displacements and hence, the values of stresses in the tank structure. Evidently, the solution of the boundary displacements involves a considerably smaller number of unknowns compared with the solution for the complete structure without partitioning. A numerical example proves the advantages of this proposed method based on the techniques of Finite Element Method (FEM). Using a program written in MatLab language, we determine the stresses in the tank structure and study its stability." @default.
- W206027655 created "2016-06-24" @default.
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- W206027655 date "2011-04-28" @default.
- W206027655 modified "2023-09-22" @default.
- W206027655 title "Plenary lecture 2: stress analysis of reinforced axisymmetrical shells using substructures" @default.
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