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This tool computes sectional properties including stiffness matrix, compliance matrix, mass matrix, and principal axes.
Thus, hierarchically enriched global stiffness matrix, mass matrix, and loading vector of general laminated plate structure are derived.
For the first time, a combined 6×6 equivalent inertia matrix (mass matrix), including both the inertia properties of the platform and the struts, is formulated parametrically.
(13 where [K ], [M], and {F} are the global stiffness matrix, mass matrix, and nodal load vector of the structure, respectively, {Q} is nodal displacement vector, and (left{ {ddot{Q}} right}) is the second derivative of the displacements of the structures with respect to time.
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Analytical formulations are developed to find the stiffness matrix, buckling stiffness matrix and mass matrix.
The stiffness matrix and mass matrix are derived, and the structural dynamics is modeled.
({mathbf {M}}), ({mathbf {K}}), ({mathbf {C}}), and ({mathbf {q}}) represent mass matrix, stiffness matrix, damping matrix, and variable vector, respectively.
From above, the derivation of dynamic FEM solution requires to determine the mass matrix, damping matrix or stiffness matrix.
In terms of structural parameters, the stiffness matrix and the mass matrix take the non-negative decomposition.
Firstly based upon the standard consistent mass matrix a special reduced bandwidth mass matrix is designed.
This method identifies the spatial matrices, namely mass matrix, damping matrix and stiffness matrix, which describe the properties of dynamic structures, using experimentally measured FRFs (Frequency Response Functions) within the frequency range of interest.
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