Issue 59
A. Behtani et alii, Frattura ed Integrità Strutturale, 59 (2022) 35-48; DOI: 10.3221/IGF-ESIS.59.03
Residual forces In this section, we explore structural damage identification based on the residual forces, details about residual forces can be found in Ref. [22]. In such approaches, the structure is divided into small elements via the finite element method, and the damage index of each element is expressed as the change of the rigidity i.e.: e e e e u d u i i i i i K K K K (14) i K is the difference in stiffness, and is a value between 0 and 1, which indicates a loss of rigidity in each element. In other words, for undamaged elements, is equal to 0, and to 1 in fully damaged elements. In this study, we assume that the damage does not affect the mass matrix of a damaged structure, therefore the rigidity matrix of the damaged element is expressed as follows: 0 1, , e e u j j j M K K j m (15) and the modal residual force vector is expressed by this equation: where u e i K and d e i K are the elementary matrices of the undamaged and damaged structures, respectively. In the above equation, Eqn. (14), e
1 2 m
e e d R K f f f f
F
e
(16)
i
i
i
m
1
2
i
As consequence, Eqn. (16) can be represented in a matrix form by the following expression:
F R
(17)
The coefficient matrix F is:
e u e d
F K
(18)
ij
j
ij
Here, ij F is the force vector in the actual node
th i on the th j element, written in the global coordinates.
The vector of residual force modal is expressed in this manner:
d
R K M d i
(19)
i
i
and Eqn. (17) is rewritten in this manner: 11 12 1 m F F F F F F
R R 1 2 1 2
m
21
22
2
(20)
F F
F
n R
m
n
n
nm
1
2
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