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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/123456789/8142
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dc.contributor.authorGoyal, Navneet-
dc.date.accessioned2022-12-26T10:47:47Z-
dc.date.available2022-12-26T10:47:47Z-
dc.date.issued1994-05-
dc.identifier.urihttps://www.sciencedirect.com/science/article/abs/pii/0020740394900477-
dc.identifier.urihttp://dspace.bits-pilani.ac.in:8080/xmlui/handle/123456789/8142-
dc.description.abstractForced axisymmetric response of a circular plate of linearly varying thickness, based on the classical theory, is analyzed by the eigen-function method. An exact solution for the free vibration mode shapes is obtained by the Frobenius method. Clamped and simply-supported plates subjected to symmetric uniformly distributed and concentrated impulsive ring and point loads are solved as example problems. Numerical results computed for transverse deflection and radial stress are plotted in the figures.en_US
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.subjectComputer Scienceen_US
dc.subjectCircular platesen_US
dc.titleForced axisymmetric response of linearly tapered circular platesen_US
dc.typeArticleen_US
Appears in Collections:Department of Computer Science and Information Systems

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