Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/333116
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dc.date.accessioned2021-07-23T04:43:28Z-
dc.date.available2021-07-23T04:43:28Z-
dc.identifier.urihttp://hdl.handle.net/10603/333116-
dc.description.abstractVisco-elastic plates are widely used in various mechanical structures, aircrafts and industries. These plates are developed with an aim that scientists and design engineers can make a use of it with a practical approach. Therefore, study of effect of vibration is of immense importance. Visco-elastic plates may be regarded as an approximation to the wings, blades and variation in thickness may also lead to reduction in weight of structure of aircraft, space shuttle or satellite. In present scenario, plates of variable thickness are used in a wide variety of applications, which serve two fold purpose i.e. safety and economy. The plates of variable thickness are being mostly used in aerospace engineering, marine engineering, mechanical engineering, civil engineering, and nuclear power plants etc. An interest towards the effect of high temperatures on non-homogeneous plates of variable thickness is developed due to applications in various fields. The reason for these is that during heating up periods, structures are exposed to high intensity heat fluxes and material properties undergo significant changes; in particular the thermal effect cannot be taken as negligible. The information about first two modes of vibration is essential for construction engineer before finalizing a design. The vibration of plates of various shapes homogeneous and non homogeneous, orthotropic or isotropic with or without variation in thickness has been studied by lot of researchers with or without considering the effect of temperature. In present study five problems have been solved on the basis of classical plate theory of elasticity. newlineIn first problem, a simple model to study the effect of non-homogeneity on vibration of parallelogram plate with bi-linear thickness variation has been represented. Thermal induced vibration of these plates has been assumed as bi-linear temperature circulation. For non-homogeneity of the plate material density is taken to be linearly varying. The governing differential equation has been solved with the help o
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dc.languageEnglish
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dc.rightsuniversity
dc.titleFree Vibration Analysis of Orthotropic SSSS Non Homogeneous Parallelogram Plate with Varying Bi Dimensional Thickness and Thermal Effect
dc.title.alternative
dc.creator.researcherManoj Kumar Dhiman
dc.subject.keywordMathematics
dc.subject.keywordPhysical Sciences
dc.description.note
dc.contributor.guideAshish Kumar Sharma
dc.publisher.placeSolan
dc.publisher.universityIEC University
dc.publisher.institutionDepartment of Mathematics
dc.date.registered2015
dc.date.completed2019
dc.date.awarded2020
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dc.format.accompanyingmaterialCD
dc.source.universityUniversity
dc.type.degreePh.D.
Appears in Departments:Department of Mathematics

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01_title.pdfAttached File86.93 kBAdobe PDFView/Open
02_certificate.pdf231.62 kBAdobe PDFView/Open
06_contents.pdf171.77 kBAdobe PDFView/Open
08_chapter 1.pdf841.76 kBAdobe PDFView/Open
09_chapter 2.pdf857.15 kBAdobe PDFView/Open
10_chapter 3.pdf803.74 kBAdobe PDFView/Open
11_chapter 4.pdf882.54 kBAdobe PDFView/Open
12_chapter 5.pdf878.67 kBAdobe PDFView/Open
13_chapter 6.pdf779.39 kBAdobe PDFView/Open
14_conclusions.pdf329.25 kBAdobe PDFView/Open
15_references.pdf192.84 kBAdobe PDFView/Open
16_publications.pdf157.42 kBAdobe PDFView/Open
80_recommendation.pdf411.74 kBAdobe PDFView/Open


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