Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/2828
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dc.contributor.authorHirwani, C. K-
dc.contributor.authorBiswas, S-
dc.contributor.authorMehar, K-
dc.contributor.authorPanda, Subrata Kumar-
dc.date.accessioned2017-12-26T12:59:14Z-
dc.date.available2017-12-26T12:59:14Z-
dc.date.issued2017-12-
dc.identifier.citation7th National Conference on Processing and Characterization of Materials-2017, NIT Rourkela, Rourkela, Odisha, 8 - 9 December, 2017en_US
dc.identifier.urihttp://hdl.handle.net/2080/2828-
dc.descriptionCopyright of this document belongs to proceedings publisher.en_US
dc.description.abstractIn this article, we investigate the thermomechanical deflection characteristics of the debonded composite plate structure using an isoparametric type of higher-order finite element model. The present mid-plane kinematics model mainly obsoletes the use of shear correction factor as in the other lower-order theories. The separation between the adjacent layers is modelled via the sub-laminate technique and the intermittent continuity conditions imposed to avoid the mathematical ill conditions. The governing equation of equilibrium of the damage plate structure under the combined state of loading are obtained using the variational principle and solved numerically to compute the defection values.en_US
dc.subjectThermomechanical deflectionen_US
dc.subjectDebonded Composite Plateen_US
dc.titleNumerical Flexural Strength Analysis of Thermally Stressed Delaminated Composite Structure under Sinusoidal Loadingen_US
dc.typePresentationen_US
Appears in Collections:Conference Papers

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