Cover image for Elasto-plastic and damage analysis of plates and shells
Title:
Elasto-plastic and damage analysis of plates and shells
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Publication Information:
Berlin : Springer, 2008
Physical Description:
xiv, 208 p. : ill. ; 24 cm.
ISBN:
9783540793502
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30000010210786 TA660.S5 V69 2008 Open Access Book Book
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Summary

Summary

Shells and plates are critical structures in numerous engineering applications. Analysis and design of these structures is of continuing interest to the scienti c and engineering communities. Accurate and conservative assessments of the maximum load carried by a structure, as well as the equilibrium path in both the elastic and inelastic range, are of paramount importance to the engineer. The elastic behavior of shells has been closely investigated, mostly by means of the nite element method. Inelastic analysis however, especially accounting for damage effects, has received much less attention from researchers. In this book, we present a computational model for nite element, elasto-plastic, and damage analysis of thin and thick shells. Formulation of the model proceeds in several stages. First, we develop a theory for thick spherical shells, providing a set of shell constitutive equations. These equations incorporate the effects of transverse shear deformation, initial curvature, and radial stresses. The proposed shell equations are conveniently used in nite element analysis. 0 AsimpleC quadrilateral, doubly curved shell element is developed. By means of a quasi-conforming technique, shear and membrane locking are prevented. The element stiffness matrix is given explicitly, making the formulation computationally ef cient. We represent the elasto-plastic behavior of thick shells and plates by means of the non-layered model, using an Updated Lagrangian method to describe a small-strain geometric non-linearity. For the treatment of material non-linearities, we adopt an Iliushin's yield function expressed in terms of stress resultants, with isotropic and kinematic hardening rules.


Table of Contents

1 Introductionp. 1
1.1 Shell Structuresp. 1
1.2 Motivation and Scopep. 4
1.3 Basic Assumptionsp. 5
Referencesp. 6
2 Shell Constitutive Equationsp. 7
2.1 Introductionp. 7
2.1.1 Thickness of the Shellp. 8
2.1.2 Initial Curvature and Radial (Transverse Normal) Stressesp. 10
2.2 Plate Constitutive Equationsp. 11
2.2.1 Stresses and Stress Resultants in a Thin Platep. 11
2.2.2 Equilibrium Equations and Governing Differential Equation of Platep. 13
2.2.3 Transverse Shear and Transverse Normal Stresses in a Platep. 15
2.3 Coordinate Transformation - Strains in Spherical Coordinatesp. 17
2.4 Theoretical Formulation of the Shell Equationsp. 22
2.4.1 Assumed Out-of-Plane Stress Componentsp. 22
2.4.2 Displacement Fieldp. 25
2.4.3 Stress Componentsp. 28
2.4.4 Stress Couples and Stress Resultants on the Middle Surfacep. 30
2.4.5 Average Displacements &ubar;, &vbar;, &wbar; and Rotations ¿¿, ¿¿p. 34
2.4.6 Equilibrium Equations and Boundary Conditionsp. 38
2.4.7 The Non-Linear Nature of the Stress Distributionp. 39
2.4.8 The Equivalent Formulation for Thick Platesp. 41
2.5 Examplesp. 41
2.5.1 Thick Sphere Subjected to Uniform Pressuresp. 42
2.5.2 Thick Cylinder Subjected to Uniform Pressuresp. 44
2.6 Summaryp. 45
Referencesp. 46
3 Shell Element Based on the Refined Theory of Thick Spherical Shellsp. 49
3.1 Introductionp. 49
3.1.1 Shear Lockingp. 49
3.1.2 Membrane Lockingp. 52
3.1.3 Mesh Instabilitiesp. 53
3.2 Finite Element Formulationp. 54
3.2.1 Shell Constitutive Equationsp. 54
3.2.2 Displacements and Boundary Conditionsp. 55
3.2.3 Element Displacement and Strain Fields - Quasi-Conforming Methodp. 57
3.2.4 Strain Energy and Stiffness Matrixp. 62
3.3 Numerical Examplesp. 64
3.3.1 The Patch Testp. 65
3.3.2 Cantilevered Beamp. 65
3.3.3 Morley's Hemispherical Shell (Morley and Moris, 1978)p. 66
3.3.4 Pinched Cylinder with Diaphragmsp. 69
3.3.5 Scordellis-Lo Roofp. 70
3.3.6 Pinched Cylinderp. 71
3.4 Summaryp. 73
Referencesp. 74
4 Geometrically Non-linear Finite Element Analysis of Thick Plates and Shellsp. 77
4.1 Introductionp. 77
4.2 Updated Lagrangian Descriptionp. 78
4.3 Shell Kinematicsp. 79
4.3.1 Local Coordinatesp. 79
4.3.2 Surface Coordinatesp. 80
4.3.3 Base Coordinatesp. 81
4.4 Explicit Tangent Stiffness Matrixp. 82
4.5 Numerical Examplep. 87
4.6 Summaryp. 89
Referencesp. 89
5 Elasto-Plastic Geometrically Non-linear Finite Element Analysis of Thick Plates and Shellsp. 91
5.1 Introductionp. 91
5.2 Yield Criterion and Hardening Rulep. 92
5.2.1 Iliushin's Yield Function (Iliushin, 1956)p. 92
5.2.2 Influence of the Shear Forcesp. 93
5.2.3 Development of the Plastic Hingep. 94
5.2.4 Bauschinger Effect and Kinematic Hardening Rulep. 94
5.3 Explicit Elasto-Plastic Tangent Stiffness Matrix with Large Displacementsp. 99
5.4 Numerical Examplesp. 106
5.4.1 Simply Supported Elasto-Plastic Beamp. 107
5.4.2 Simply Supported Platep. 108
5.4.3 Cylindrical Shell Subjected to Ring of Pressurep. 112
5.4.4 Spherical Dome Subjected to Ring of Pressurep. 114
5.5 Summaryp. 115
Referencesp. 116
6 Elasto-Plastic Geometrically Non-linear Finite Element Analysis of Thick Plates and Shells With Damage Due to Microvoidsp. 119
6.1 Introductionp. 119
6.2 Yield and Damage Criterionp. 121
6.3 Explicit Tangent Stiffness Matrixp. 128
6.4 Numerical Examplesp. 135
6.4.1 Clamped Square Plate Subjected to a Central Point Loadp. 136
6.4.2 Spherical Dome Subjected to Ring of Pressurep. 137
6.5 Summaryp. 139
Referencesp. 141
7 Non-linear Post Buckling Finite Element Analysis of Plates and Shellsp. 145
7.1 Introductionp. 145
7.2 Element Tangent Stiffness Matrixp. 146
7.2.1 Element Stiffness in Local Coordinatesp. 146
7.2.2 Initial Surface Coordinates for Large Deformation Analysisp. 150
7.2.3 Transformation of Element Stiffness Matrixp. 151
7.3 Solution Algorithmp. 152
7.4 Numerical Examplesp. 153
7.4.1 The Williams' Toggle Framep. 153
7.4.2 Simply Supported Circular Plate Subjected to Edge Pressurep. 154
7.4.3 Rectangular Plate Subjected to In-Plane Loadp. 155
7.4.4 Cylindrical Shell Under a Central Loadp. 157
7.4.5 Spherical Shell Subjected to Central Loadp. 159
7.5 Summaryp. 160
Referencesp. 160
8 Determination of Transverse Shear Stresses and Delamination in Composite Laminates Using Finite Elementsp. 163
8.1 Introductionp. 163
8.2 Kinematics of the Shellp. 164
8.3 Lamina Constitutive Equationsp. 166
8.4 Failure Criteria for Composite Laminatesp. 171
8.5 Implementation and Numerical Examplesp. 172
8.5.1 Laminated Composite Strip under Three-Point Bendingp. 173
8.5.2 Composite Cylinder under Internal Pressurep. 178
8.5.3 Cylindrical Shell Subjected to Ring of Pressurep. 180
8.6 Summaryp. 182
Referencesp. 183
9 Numerical Methods and Computational Algorithmsp. 185
9.1 Introductionp. 185
9.2 Linear Elastic Analysis - System of Linear Algebraic Equationsp. 185
9.3 Non-linear Analysis - System of Non-linear Algebraic Equationsp. 187
9.3.1 Modified Newton-Raphson Method - Combined Incremental/Iterative Solutionsp. 188
9.3.2 The Arc-Length Techniquep. 190
9.3.3 Integrating the Rate Equations - Return to the Yield Surfacep. 194
Referencesp. 196
Appendixp. 199
Indexp. 201