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Shock and Vibration
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Shock and Vibration
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2016
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Article
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Fig 24
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Research Article
Hermitian Mindlin Plate Wavelet Finite Element Method for Load Identification
Figure 24
The absolute error with excitation
applied at nodes 9 and 26.
(a)
Identified load
at node 9
(b)
Identified load
at node 26