Please use this identifier to cite or link to this item: https://dspace.iiti.ac.in/handle/123456789/10593
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dc.contributor.authorSingh, Sandeepen_US
dc.date.accessioned2022-07-19T14:16:09Z-
dc.date.available2022-07-19T14:16:09Z-
dc.date.issued2022-
dc.identifier.citationWatts, G., Kumar, R., Singh, S., Sengar, V., Reddy, G. R., & Patel, S. N. (2022). Postbuckling and postbuckled vibration behaviour of imperfect trapezoidal sandwich plates with FG-CNTRC face sheets under nonuniform loadings. Aerospace Science and Technology, 127, 107716. https://doi.org/10.1016/j.ast.2022.107716en_US
dc.identifier.issn1270-9638-
dc.identifier.otherEID(2-s2.0-85133471788)-
dc.identifier.urihttps://doi.org/10.1016/j.ast.2022.107716-
dc.identifier.urihttps://dspace.iiti.ac.in/handle/123456789/10593-
dc.description.abstractThe present work investigates the postbuckling, and postbuckled vibration behaviour of initially imperfect trapezoidal sandwich plates with functionally graded carbon nanotube reinforced composite (FG-CNTRC) face sheets and FG porous metal foam core under the influence of non-uniform edge compression. The plate's kinematic assumptions are based on a refined higher order theory and the strain-displacement relations include von Karman assumptions for geometrical nonlinearity. The weak form of governing equations derived using Hamilton's principle is transformed into a discretized form of algebraic equations using the element free Galerkin (EFG) method in conjunction with moving kriging (MK) interpolation functions. The pre-buckling stresses are determined using static analysis to evaluate accurate critical buckling loads. Modified Riks technique is used to trace nonlinear equilibrium paths. Parametric studies include the effect of CNT distribution in face sheets, porosity distribution in the core layer and edge loading conditions on the nonlinear stability and vibration behaviour of sandwich plates. New results on trapezoidal sandwich plates with initial imperfections, hitherto not found in the literature, are presented for the first time, which can be used as benchmark solutions for further research. © 2022 Elsevier Masson SASen_US
dc.language.isoenen_US
dc.publisherElsevier Masson s.r.l.en_US
dc.sourceAerospace Science and Technologyen_US
dc.subjectAlgebraen_US
dc.subjectCarbon nanotubesen_US
dc.subjectControl nonlinearitiesen_US
dc.subjectGalerkin methodsen_US
dc.subjectMetal foamsen_US
dc.subjectMetalsen_US
dc.subjectVibrations (mechanical)en_US
dc.subjectCarbon nanotubes reinforced compositesen_US
dc.subjectElement-free Galerkin methoden_US
dc.subjectFunctionally gradeden_US
dc.subjectFunctionally graded carbon nanotube reinforced composite plateen_US
dc.subjectKrigingen_US
dc.subjectMoving kriging shape functionen_US
dc.subjectPostbucklingen_US
dc.subjectReinforced composite platesen_US
dc.subjectSandwich platesen_US
dc.subjectShape functionsen_US
dc.subjectTrapezoidal platesen_US
dc.subjectKrigingen_US
dc.titlePostbuckling and postbuckled vibration behaviour of imperfect trapezoidal sandwich plates with FG-CNTRC face sheets under nonuniform loadingsen_US
dc.typeJournal Articleen_US
Appears in Collections:Department of Mechanical Engineering

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