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56 Damage Detection on Structures of Offshore <strong>Wind</strong> Turbines 303<br />

Table 56.1. Identified stiffness parameters by means of measured (simulated)<br />

eigenfrequencies with an accuracy of three correct decimal places<br />

Measured eigenfrequencies (Hz) Determined stiffness parameters (–)<br />

0.407<br />

2.782<br />

7.618<br />

� †<br />

A<br />

∆0 = det 11 A† 12<br />

A †<br />

21 A†<br />

22<br />

�<br />

1.002<br />

0.897<br />

1.003<br />

= A †<br />

11A† 22 − A† 21A† 12 . (56.6)<br />

It is shown in [3] that the development of determinants using Cramers Rule<br />

and the application of the cofactor to (56.5) lead to a problem which is equivalent<br />

to (56.1)<br />

∆pfq − ∆qfp =0. (56.7)<br />

With a non-singular linear combination of the determinantal maps one obtains<br />

linear eigenvalue problems for the model parameters<br />

fs = ∆ −1 ∆sf = λsf. (56.8)<br />

These problems are well-posed. There is no incompleteness of information<br />

because the number of required eigenfrequencies depends only on the number<br />

of stiffness parameters.<br />

Numerical Example: In the current state of method validation, measurement<br />

data are not yet available. Therefore, artificial measurement data are<br />

generated by applying scatter to the exact eigenfrequencies as resulting from<br />

the analysis. It is supposed that the middle area of a cantilever beam model<br />

with three elements (denoted by one to three beginning from the bottom) and<br />

nine DOF has a stiffness degradation of 10%. In the first column of Table 56.1<br />

the first three eigenfrequencies for the bending modes are shown with an accuracy<br />

of three correct decimal places. The solution of the eigenvalue problems<br />

determines the set of stiffness parameters as shown in the second column. A<br />

stiffness parameter equal to one refers to an undamaged structural element.<br />

The decrease of the second stiffness parameter points to a damage in this<br />

region. The value of 0.897 indicates a stiffness reduction of 10.3% which is<br />

quite close to the damage applied before. Furthermore, damage of the correct<br />

structural element is reflected since the stiffness parameters of elements one<br />

and three remain almost identical to one.<br />

56.3 Validation of the Method<br />

A validation of the method by means of a sensitivity analysis was carried out.<br />

Therewith the influence of several parameters of the method on the accuracy<br />

of the quantification was investigated. The parameters of the method

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