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Stiffness and mass matrices of the laminate.
Stiffness as well as mass matrices of the curved and the straight beam elements is formulated.
The stiffness and mass matrices of the shell are derived analytically.
It uses only the stiffiness and mass matrices of each substructure.
The stiffness and mass matrices of the element are obtained by Carrera's Unified Formulation (CUF).
The stiffness and mass matrices of elements are obtained by Carrera's Unified Formulation (CUF).
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Mass matrix of the system.
Mass matrix of equivalent model can be calculated considering degrees of freedom for each storey.
These conditions result in a set of general inequalities for the elements of the mass matrix of every mesh element.
The proposed methods are based on the results from the modal analysis of the original structure, and the stiffness and mass matrix of the modified structures.
The related contents cover the expression of displacement field, the stiffness matrix and the consistent mass matrix of beam element, and transformation matrix.
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