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http://hdl.handle.net/10603/228067
Title: | Studies on moderately thick composite sector plates |
Researcher: | Sharma, Ashish |
Guide(s): | Sharda, H. B. and Nath Y. |
Keywords: | Applied mechanics Buckling Chebyshev polynomials Cylindrical orthotropy Free vibration Large deformation Mindlin sector plate Non-linear transient response |
University: | Thapar Institute of Engineering and Technology |
Completed Date: | 2005 |
Abstract: | Rapid advancements made in materials science and manufacturing technologies has lead to the application of composite materials in various areas of engineering applica-tions like aerospace industries, marine structures, automobiles, power plant systems etc. The composite materials are often subjected to severe operating conditions with respect to kinds of loadings, temperature variations, vibration, shocks etc. The struc-tural configurations could be in various shapes, the most common being in the form of plates and shells. The plates can be of rectangular, circular, sectoral or of any other shape. There are different kinds of important and complicated phenomena like bend-ing, buckling, vibration etc. associated with these structural elements. Therefore, it is necessary to study adequately these aspects for accurate design estimates. The models studied could be linear for small deformation analysis in linearly elas-tic range. For large deformation analysis or for non-linear constitutive relationships, the model is non-linear. The stringent operating conditions often lead to deforma-tions comparable to plate thickness. This necessitates the application of geometrically non-linear formulations. The computational effort is reduced by reducing the general three dimensional problem to planar problem with the use of different kinds of plate theories. The formulation analyzed in this thesis applies the FSDT and takes in to account von-K´arm´an type of non-linearities. The differential equations governing the behavior of sector plates are more compli-cated as compared to other geometrical configurations. The present thesis attempts to study the behavior of laminated plates in sectoral domain using fast converging Chebyshev polynomials. The linear eigenvalue problems of buckling and free vibration of isotropic and lam-inated composite plates are studied. The non-linear algebraic equations generated from the static large deformation analysis are solved using an incremental iterative scheme based on Newton-Raphson technique. |
Pagination: | xxvi, 133 |
URI: | http://hdl.handle.net/10603/228067 |
Appears in Departments: | Department of Mechanical Engineering |
Files in This Item:
File | Description | Size | Format | |
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file10(chapter 7).pdf | Attached File | 347.55 kB | Adobe PDF | View/Open |
file11(chapter 8).pdf | 223.33 kB | Adobe PDF | View/Open | |
file12(chapter 9).pdf | 48.01 kB | Adobe PDF | View/Open | |
file13(references).pdf | 72.22 kB | Adobe PDF | View/Open | |
file14(appendix).pdf | 73.74 kB | Adobe PDF | View/Open | |
file1(title).pdf | 36.11 kB | Adobe PDF | View/Open | |
file2(certificate).pdf | 144.08 kB | Adobe PDF | View/Open | |
file3(preliminary pages).pdf | 660.3 kB | Adobe PDF | View/Open | |
file4(chapter 1).pdf | 138.55 kB | Adobe PDF | View/Open | |
file5(chapter 2).pdf | 132.39 kB | Adobe PDF | View/Open | |
file6(chapter 3).pdf | 504.67 kB | Adobe PDF | View/Open | |
file7(chapter 4).pdf | 203.31 kB | Adobe PDF | View/Open | |
file8(chapter 5).pdf | 335.09 kB | Adobe PDF | View/Open | |
file9(chapter 6).pdf | 195.76 kB | Adobe PDF | View/Open |
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