Comprehensive literature reviews on buckling of composite laminated plates were presented and discussed thoroughly.Exact,analytical and semi-analytical solution techniques were compared and analyzed using different factors which include boundary conditions,plate dimensions and lamination scheme.Development of plate theories was considered in the analysis of buckling.It was found that there are two main theories of laminated plates which are known as linear and nonlinear theories.The two theories are depending on the magnitude of deformation resulting from loading the given plates.The difference between the two theories is that the deformations are small in the linear theory,whereas they are finite or large in the nonlinear theory.It was also found that higher order shear deformation theories can yield more accurate inter-laminate stresses and also avoids the need for shear correction displacement.In comparison between finite element method (FEM) and different numerical methods,it was found that FEM could be considered of acceptable accuracy,and could also be applied to different complicated geometries and shapes.
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Comprehensive literature reviews on buckling of composite laminated plates were presented and discussed thoroughly.Exact,analytical and semi-analytical solution techniques were compared and analyzed using different factors which include boundary conditions,plate dimensions and lamination scheme.Development of plate theories was considered in the analysis of buckling.It was found that there are two main theories of laminated plates which are known as linear and nonlinear theories.The two theories are depending on the magnitude of deformation resulting from loading the given plates.The difference between the two theories is that the deformations are small in the linear theory,whereas they are finite or large in the nonlinear theory.It was also found that higher order shear deformation theories can yield more accurate inter-laminate stresses and also avoids the need for shear correction displacement.In comparison between finite element method (FEM) and different numerical methods,it was found that FEM could be considered of acceptable accuracy,and could also be applied to different complicated geometries and shapes.
Osama Mohammed Elmardi was born in Atbara-Sudan in 1966. He received Bachelor degree in Mechanical Engineering from Sudan University of Science and Technology in 1998,and a Master degree in solid mechanics from Nile Valley University in 2003. He supervised more than 200 final students' projects in Master, Bachelor and Diploma degrees.
Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.
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 -Comprehensive literature reviews on buckling of composite laminated plates were presented and discussed thoroughly.Exact,analytical and semi-analytical solution techniques were compared and analyzed using different factors which include boundary conditions,plate dimensions and lamination scheme.Development of plate theories was considered in the analysis of buckling.It was found that there are two main theories of laminated plates which are known as linear and nonlinear theories.The two theories are depending on the magnitude of deformation resulting from loading the given plates.The difference between the two theories is that the deformations are small in the linear theory,whereas they are finite or large in the nonlinear theory.It was also found that higher order shear deformation theories can yield more accurate inter-laminate stresses and also avoids the need for shear correction displacement.In comparison between finite element method (FEM) and different numerical methods,it was found that FEM could be considered of acceptable accuracy,and could also be applied to different complicated geometries and shapes. 60 pp. Englisch. N° de réf. du vendeur 9783659863875
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Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Osama Mohammed ElmardiOsama Mohammed Elmardi was born in Atbara-Sudan in 1966. He received Bachelor degree in Mechanical Engineering from Sudan University of Science and Technology in 1998,and a Master degree in solid mechanics from . N° de réf. du vendeur 158248436
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Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -Comprehensive literature reviews on buckling of composite laminated plates were presented and discussed thoroughly.Exact,analytical and semi-analytical solution techniques were compared and analyzed using different factors which include boundary conditions,plate dimensions and lamination scheme.Development of plate theories was considered in the analysis of buckling.It was found that there are two main theories of laminated plates which are known as linear and nonlinear theories.The two theories are depending on the magnitude of deformation resulting from loading the given plates.The difference between the two theories is that the deformations are small in the linear theory,whereas they are finite or large in the nonlinear theory.It was also found that higher order shear deformation theories can yield more accurate inter-laminate stresses and also avoids the need for shear correction displacement.In comparison between finite element method (FEM) and different numerical methods,it was found that FEM could be considered of acceptable accuracy,and could also be applied to different complicated geometries and shapes.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 60 pp. Englisch. N° de réf. du vendeur 9783659863875
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Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Comprehensive literature reviews on buckling of composite laminated plates were presented and discussed thoroughly.Exact,analytical and semi-analytical solution techniques were compared and analyzed using different factors which include boundary conditions,plate dimensions and lamination scheme.Development of plate theories was considered in the analysis of buckling.It was found that there are two main theories of laminated plates which are known as linear and nonlinear theories.The two theories are depending on the magnitude of deformation resulting from loading the given plates.The difference between the two theories is that the deformations are small in the linear theory,whereas they are finite or large in the nonlinear theory.It was also found that higher order shear deformation theories can yield more accurate inter-laminate stresses and also avoids the need for shear correction displacement.In comparison between finite element method (FEM) and different numerical methods,it was found that FEM could be considered of acceptable accuracy,and could also be applied to different complicated geometries and shapes. N° de réf. du vendeur 9783659863875
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Taschenbuch. Etat : Neu. Introduction and Literature Review on Buckling of Composite Laminates | Mohammed Elmardi Osama | Taschenbuch | 60 S. | Englisch | 2016 | LAP LAMBERT Academic Publishing | EAN 9783659863875 | 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 103851286
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