Finite Element Analysis of Shell Structures - Couverture souple

Mohamed Adam, Fathelrahman; Elzubair Mohamed, AbdelRahman

 
9783659381584: Finite Element Analysis of Shell Structures
Couverture souple
ISBN 10 : 3659381586 ISBN 13 : 9783659381584
Editeur : LAP LAMBERT Academic Publishing, 2013

Synopsis

The finite element analysis of general shell structures is faced with the problems of shear and membrane locking. These problems are well known and much research has been focused on the development of powerful shell elements to eliminate these problems. This book employs three shell elements these are four nodes degenerated shell element, four nodes flat shell element and nine nodes degenerated shell element. Each one of these elements has six degrees of freedom per node. Additional elements have been developed to avoid problems; these are: four nodes element, employing the Mixed Interpolation of Tensorial Components approach, Non Conforming Element and nine nodes element with Selective Reduced Integration and Weighted Modified Integration. A new solution is proposed to correct the convergence curve to be asymptotic to the exact solution curve by using extrapolation. A geometric nonlinear formulation based on the total Lagrangian formulation using both engineering strains and Green’s strains was adopted. The formulations were implemented into a nonlinear finite element program and some subroutines are included. Good results are obtained when applying in different numerical examples

Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.

Présentation de l'éditeur

The finite element analysis of general shell structures is faced with the problems of shear and membrane locking. These problems are well known and much research has been focused on the development of powerful shell elements to eliminate these problems. This book employs three shell elements these are four nodes degenerated shell element, four nodes flat shell element and nine nodes degenerated shell element. Each one of these elements has six degrees of freedom per node. Additional elements have been developed to avoid problems; these are: four nodes element, employing the Mixed Interpolation of Tensorial Components approach, Non Conforming Element and nine nodes element with Selective Reduced Integration and Weighted Modified Integration. A new solution is proposed to correct the convergence curve to be asymptotic to the exact solution curve by using extrapolation. A geometric nonlinear formulation based on the total Lagrangian formulation using both engineering strains and Green’s strains was adopted. The formulations were implemented into a nonlinear finite element program and some subroutines are included. Good results are obtained when applying in different numerical examples

Biographie de l'auteur

Fathelrahman M. Adam Assistance professor, Department of Civil Engineering, Jazan University. Studied civil engineering at Sudan University of Science and Technology and received his post graduate studies at the same university. For many years he taught courses on structural analysis and R.C. Design and work as structural engineering consultant.

Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.

Éditeur
LAP LAMBERT Academic Publishing
Date d'édition
2013
Langue
anglais
ISBN 10 
3659381586
ISBN 13 
9783659381584
Reliure
Broché
Nombre de pages
232
Coordonnées du fabricant
non disponible
Personne responsable
KreGa Onlinehandel GmbH
4950000000000
info@krega-onlinehandel.de

Birkenweg 31
Brakel
33034
Allemagne