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DC Field | Value | Language |
---|---|---|
dc.contributor.author | Kumar, Rajesh | - |
dc.date.accessioned | 2024-04-26T08:57:38Z | - |
dc.date.available | 2024-04-26T08:57:38Z | - |
dc.date.issued | 2022-06 | - |
dc.identifier.uri | https://www.tandfonline.com/doi/full/10.1080/15376494.2022.2085827 | - |
dc.identifier.uri | http://dspace.bits-pilani.ac.in:8080/jspui/xmlui/handle/123456789/14688 | - |
dc.description.abstract | The non-linear dynamic response of a randomly distributed carbon nanotube fiber-reinforced laminated composite (CNTFRLC) plate subjected to various in-plane pulse localized loadings and transverse patch loading is presented semi-analytically. Implementing higher-order shear deformation theory (HSDT) along with von-Kármán non-linearity, the non-linear kinematics of the CNTFRLC plate are modeled. The nonuniform pre-buckling stresses (σxx, σyy, and τxy) were developed implementing Airy’s stress equilibrium approach, and subsequently utilized while deriving the non-linear partial differential equations (PDEs) of the plate through Hamilton’s principle and solved via. Galerkin’s method. Finally, the non-linear dynamic responses of the CNTFRLC plate are traced using Newmark’s method. | en_US |
dc.language.iso | en | en_US |
dc.publisher | Taylor & Francis | en_US |
dc.subject | Civil Engineering | en_US |
dc.subject | CNT fiber-reinforced laminated composite (CNTFRLC) plate | en_US |
dc.subject | Eshelby-Mori-Tanaka scheme | en_US |
dc.subject | Galerkin’s Method | en_US |
dc.subject | Pulse Force | en_US |
dc.subject | Non-Linear Dynamic Response | en_US |
dc.title | A semi-analytical framework for non-linear dynamic response of multi-phase laminated composite plate under the transverse patch and in-plane pulse localized loadings | en_US |
dc.type | Article | en_US |
Appears in Collections: | Department of Civil Engineering |
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