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Автор Tutuncu, Naki
Дата выпуска 1998
dc.description Stresses and deformations due to a uniform change in temperature in plates of general polar anisotropy are determined. The plate was assumed to be symmetrically laminated, each lamina being oriented at an arbitrary angle with respect to the radial coordinate. Due to unconstrained and stress-free outer boundary of the plate, derivation of a closed-form solution for radial and circumferential displacements was possible. The interlaminar thermal stresses are then calculated and, using the Tsai-Wu tensorial failure theory, the reserve factors for each lamina interface has been determined. The material used for numerical results was chosen arbitrarily for purely illustration purposes. The results have shown that it was preferable, solely for the increased strength purposes, to have circumferentially wound fibers for the particular material and the lay-up chosen.
Издатель TECHNOMIC PUBLISHING CO., INC.
Название Interlaminar Thermal Stresses in Polar-Anisotropic Circular Plates
Тип Journal Article
DOI 10.1177/073168449801701104
Print ISSN 0731-6844
Журнал Journal of Reinforced Plastics and Composites
Том 17
Первая страница 1024
Последняя страница 1035
Аффилиация Tutuncu, Naki, Department of Mechanical Engineering, Cukurova University, 01330 Adana, Turkey
Выпуск 11
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