Issue 54
F. Brandão et alii, Frattura ed Integrità Strutturale, 54 (2020) 66-87; DOI: 10.3221/IGF-ESIS.54.05
In which M , C and K represent the (n+N TMD )x(n+N TMD ) mass, stiffness and damping matrices and n is the number of degrees of freedom. The damping matrix C is assumed to be proportional to the M and K matrices as: C = α M + β K . , u(t) , u(t) , u(t) are the (n+N TMD )- dimensional acceleration, velocity and displacement vectors relative to ground, respectively. The matrix B is a (n+N TMD )xd matrix that contains the cosine directors of the angles formed between the base motion and the associated displacement direction with the considered degree of freedom and d is the number of considered ground motions (directions). , g u (t) represents the base acceleration and is a d -dimensional vector.
Figure 1: n-degree-of-freedom system (n-DOF) structure equipped (a) with one TMD at the top floor and (b) with MTMD possibly located in all floors of the structure. In Fig. 1.(a), there is a single TMD attached at the top floor of the structure. The structure DOF is increased by one and the TMD contribution to M and K , is illustrated in Eqns. 2 and 3. For the C matrix, the procedure is analogous to the K .
m
1 2 0 0 m
0 0 0 0
M
(2)
m
0 0 0 0
0
n
m
0
TMD
k k k
0 0
0 0
1
2
2
k k k
2
2
3
K
(3)
k k
k
0 0
0 0
n
TMD TMD
k
k
TMD
TMD
Fig. 1.(b) represents the MTMD possibly located on all floors of the structure, the TMD contribution to M and K is illustrated in Eqns. 4 and 5. Again, for the C matrix, the procedure is analogous to the K .
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