Shock and Vibration / 2019 / Article / Fig 9

Research Article

Operational Deflection Shape Extraction from Broadband Events of an Aircraft Component Using 3D-DIC in Magnified Images

Figure 9

ODSs of the window in the out-of-plane direction, W, obtained with 3D-DIC in forced normal mode tests for the resonances: (a) 124 Hz and (b) 215 Hz.

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