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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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Tab 3
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Research Article
Nonlinear Modeling and Identification of an Aluminum Honeycomb Panel with Multiple Bolts
Table 3
Experimentally measured, initial, and updated natural frequencies.
Natural frequency
Experimental value
Initial value
Updated value
14.63
23.6
14.63
104.02
149.38
102.86
144.40
189.89
137.62