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Please use this identifier to cite or link to this item: http://dspace.bits-pilani.ac.in:8080/jspui/xmlui/handle/123456789/14682
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dc.contributor.authorKumar, Rajesh-
dc.date.accessioned2024-04-25T10:14:12Z-
dc.date.available2024-04-25T10:14:12Z-
dc.date.issued2022-12-
dc.identifier.urihttps://www.sciencedirect.com/science/article/pii/S0997753822001917-
dc.identifier.urihttp://dspace.bits-pilani.ac.in:8080/jspui/xmlui/handle/123456789/14682-
dc.description.abstractIn this study, the buckling and free vibration characteristics of three-phase randomly distributed carbon nanotube (CNT) reinforced fiber composite (RD-CNTRFC) beams subjected to in-plane compressive loadings and thermal environment are discussed in-depth through a semi-analytical approach. Displacement-based governing equations of motion are derived using Lagrange equation considering higher-order shear deformation theory (HSDT). The effective material properties of RD-CNTRFC are determined in two stages; firstly, effective properties of hybrid matrix (CNTs + Polymer) are evaluated using the Eshelbhy-Mori-Tanaka approach. Finally, overall effective properties of CNTRFC are estimated by implementing different homogenization techniques. The influences of temperature-dependent material properties and CNT-agglomeration are included in the derived formulation. The buckling loads and natural frequencies of RD-CNTRFC beams are computed using a typical eigenvalue solution. The influence of various boundary conditions, CNT mass fraction, CNT-agglomeration, length-to-thickness ratio, and various ply sequences are also addressed.en_US
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.subjectCivil Engineeringen_US
dc.subjectBucklingen_US
dc.subjectVibrationsen_US
dc.subjectCarbon nanotubeen_US
dc.subjectThermomechanical loadingen_US
dc.titleBuckling and free vibration analysis of randomly distributed CNT reinforced composite beam under thermomechanical loadingen_US
dc.typeArticleen_US
Appears in Collections:Department of Civil Engineering

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