The increasing use of the laminated composite plates in the construction of mechanical, aerospace, marine, and automotive structures has made the design of these laminates an important research topic. One of the most important reasons for using laminated composite materials in these applications is to reduce the structural weight. Consequently, the main objective of this thesis is to find the minimum weight design of the laminated plates under the application of dynamic loads and subject to different flexibility and strength constraints. The common objective in the optimal design of laminated composite plates is to determine layer orientation, layer thicknesses, or number of layers to obtain the minimum weight of the structure and to satisfy the imposed constraints. In this work the ply thicknesses are taken as a continuous design variables. The optimal ply orientation and the optimal lamination scheme are determined through a parametric study according to the boundary conditions of the problem and the aspect ratio of the plate.
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Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne
Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The increasing use of the laminated composite plates in the construction of mechanical, aerospace, marine, and automotive structures has made the design of these laminates an important research topic. One of the most important reasons for using laminated composite materials in these applications is to reduce the structural weight. Consequently, the main objective of this thesis is to find the minimum weight design of the laminated plates under the application of dynamic loads and subject to different flexibility and strength constraints. The common objective in the optimal design of laminated composite plates is to determine layer orientation, layer thicknesses, or number of layers to obtain the minimum weight of the structure and to satisfy the imposed constraints. In this work the ply thicknesses are taken as a continuous design variables. The optimal ply orientation and the optimal lamination scheme are determined through a parametric study according to the boundary conditions of the problem and the aspect ratio of the plate. 120 pp. Englisch. N° de réf. du vendeur 9783847332916
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Vendeur : moluna, Greven, Allemagne
Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Kabeel AbdallahA. M. Kabeel received his B.S, and M.S.in Mechanical Engineering from ZagazigUniversity, Egypt in 1999 and 2007,respectively. A.M. Kabeel is currentlyan assistance lecturer of the Departmentof Mechanical Design and Pro. N° de réf. du vendeur 5510702
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Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The increasing use of the laminated composite plates in the construction of mechanical, aerospace, marine, and automotive structures has made the design of these laminates an important research topic. One of the most important reasons for using laminated composite materials in these applications is to reduce the structural weight. Consequently, the main objective of this thesis is to find the minimum weight design of the laminated plates under the application of dynamic loads and subject to different flexibility and strength constraints. The common objective in the optimal design of laminated composite plates is to determine layer orientation, layer thicknesses, or number of layers to obtain the minimum weight of the structure and to satisfy the imposed constraints. In this work the ply thicknesses are taken as a continuous design variables. The optimal ply orientation and the optimal lamination scheme are determined through a parametric study according to the boundary conditions of the problem and the aspect ratio of the plate. N° de réf. du vendeur 9783847332916
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Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne
Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -The increasing use of the laminated composite plates in the construction of mechanical, aerospace, marine, and automotive structures has made the design of these laminates an important research topic. One of the most important reasons for using laminated composite materials in these applications is to reduce the structural weight. Consequently, the main objective of this thesis is to find the minimum weight design of the laminated plates under the application of dynamic loads and subject to different flexibility and strength constraints. The common objective in the optimal design of laminated composite plates is to determine layer orientation, layer thicknesses, or number of layers to obtain the minimum weight of the structure and to satisfy the imposed constraints. In this work the ply thicknesses are taken as a continuous design variables. The optimal ply orientation and the optimal lamination scheme are determined through a parametric study according to the boundary conditions of the problem and the aspect ratio of the plate.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 120 pp. Englisch. N° de réf. du vendeur 9783847332916
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Vendeur : preigu, Osnabrück, Allemagne
Taschenbuch. Etat : Neu. Optimal Design of Laminated Plates Subjected to Dynamic Loads | Composite plates analysis and optimization | Abdallah Kabeel | Taschenbuch | 120 S. | Englisch | 2012 | LAP LAMBERT Academic Publishing | EAN 9783847332916 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. N° de réf. du vendeur 106669361
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