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Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/313
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dc.contributor.authorPatel, G-
dc.contributor.authorSahu, S K-
dc.date.accessioned2006-08-04T04:28:18Z-
dc.date.available2006-08-04T04:28:18Z-
dc.date.issued2006-
dc.identifier.citationNational Conference on “Emerging Trends in Nano Technology and innovations in design and manufacturing, Feb 18-19, 2006, NIT, Rourkela, Indiaen
dc.identifier.urihttp://hdl.handle.net/2080/313-
dc.descriptionCopyright for this article belongs to the proceedings publisheren
dc.description.abstractThe static stability of the curved panels subjected to varieties of non-uniform loading including partial and concentrated in-plane compressive edge loading is studied using finite element method, considering the effects of transverse shear deformation and rotary inertia. An eight nodded quadratic isoparametric element is employed in the present analysis. The study reveals that the stability behaviour of the flat and curved panels is greatly influenced by the geometry, boundary conditions, the type and position of loadsen
dc.format.extent597442 bytes-
dc.format.mimetypeapplication/pdf-
dc.language.isoen-
dc.publisherNIT Rourkelaen
dc.subjectBucklingen
dc.subjectCurved Panelen
dc.subjectFinite Element Methoden
dc.subjectNon-uniform Loaden
dc.titleBuckling of Curved Panels Subjected to Non-uniform Loading Using Finite Element Methoden
dc.typeArticleen
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