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Principal component analysis and perturbation theory–based robust damage detection of multifunctional aircraft structure

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Academic year: 2021

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Figure

Figure 1: Antenna of the AIRBUS A318 [5]
Table 1: Mechanical properties of the composite material
Figure 2: Finite element model of a composite plate bounded with piezoceramic patches
Figure 4: Visualization manner of the damage decision: composite plate model
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