International Journal of Aerospace Engineering / 2018 / Article / Tab 6

Research Article

Structural Damage Detection Using Nonlinear Vibrations

Table 6

Number of superharmonic peaks () and maximum superharmonic frequency content ().

Case, node 12, node 12 (Hz), node 93, node 93 (Hz)

Reference7160260
D228024980
D326026820
D5197009820

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