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Effect of Cutout on the Stability and Failure of Laminated Composite Cylindrical Panels Subjected to In-Plane Pulse Loads

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dc.contributor.author Patel, S. N.
dc.contributor.author Kumar, Rajesh
dc.date.accessioned 2022-12-17T13:48:27Z
dc.date.available 2022-12-17T13:48:27Z
dc.date.issued 2022
dc.identifier.uri https://www.worldscientific.com/doi/10.1142/S0219455422500870
dc.identifier.uri http://dspace.bits-pilani.ac.in:8080/xmlui/handle/123456789/7898
dc.description.abstract In this investigation, the nonlinear dynamic buckling analysis and the failure analysis of laminated composite cylindrical (LCC) panel with different shapes of cutouts under the action of rectangular in-plane pulse loads are performed in the finite element framework. Cross-ply laminates which are balanced symmetric are considered in the investigation. The first ply failure load (FPFL) of the panel is evaluated and checked whether it occurs before the nonlinear dynamic buckling phenomenon considering Tsai–Wu failure criterion. Convergence and validation studies are undertaken, and the results are compared with those from the existing literature. The effects of loading duration, cutout area and cutout geometry on the panel are investigated in detail and results are reported. The results indicate that for the panel with cutout, its dynamic buckling load (DBL), in certain cases, compared to the static buckling load (SBL), can be lower even if the loading duration is half of its first natural period. Additionally, the vibration and the static buckling analyses of the panels are carried out as and when required. en_US
dc.language.iso en en_US
dc.publisher World Scientific en_US
dc.subject Civil Engineering en_US
dc.subject In-plane pulse loads en_US
dc.subject Dynamic buckling en_US
dc.subject Cylindrical panels en_US
dc.subject Composite laminates en_US
dc.subject Cutouts en_US
dc.title Effect of Cutout on the Stability and Failure of Laminated Composite Cylindrical Panels Subjected to In-Plane Pulse Loads en_US
dc.type Article en_US


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