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Shock and Vibration
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Shock and Vibration
/
2019
/
Article
/
Tab 3
/
Research Article
A Simplified Finite Element Approach for Modeling of Multilayer Plates
Table 3
Comparison of loss factor between the data in Kung and Singh [
22
] and new plate finite element.
Mode
Results of Kung and Singh [
22
]
New element
Difference (%)
(1, 1)
0.044
0.051
15.9
(1, 2)
0.019
0.021
10.5
(2, 1)
0.019
0.021
10.5
(2, 2)
0.012
0.013
8.3