Use of Statical Indentation Laws in the Impact Analysis of Laminated Composite Plates
Keyword(s):
The low-velocity impact response of graphite/epoxy laminates was investigated theoretically and experimentally. A nine-node isoparametric plate finite element in conjunction with an empirical contact law was used for the theoretical investigation. Theoretical results are in good agreement with strain-gage experimental data. The results of the investigation indicate that the present theoretical procedure describes the impact response of laminate for low-impact velocities.
Low velocity impact analysis of laminated composite plates using a 3D elasticity based layerwise FEM
2009 ◽
Vol 30
(9)
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pp. 3795-3801
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2020 ◽
Vol 42
(6)
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2003 ◽
Vol 12
(5)
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pp. 096369350301200
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2003 ◽
Vol 59
(1)
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pp. 119-127
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2011 ◽
Vol 93
(5)
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pp. 1363-1375
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2017 ◽
Vol 25
(9)
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pp. 677-682
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2014 ◽
Vol 629
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pp. 503-506
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