Erasmo Carrera, Maria Cinefra, Marco Petrolo, Enrico Zappino

Finite Element Analysis of Structures Through Unified Formulation

• Gebundenes Buch

Produktbeschreibung

This book deals with the Finite Element Method for the analysis of elastic structures such as beams, plates, shells and solids. The modern approach of Unified Formulation (UF), as proposed by the lead author, deals with the consideration of one-dimensional (beams), two-dimensional (plates and shells) and three-dimensional (solids) elements. Applications are given for structures which are typically employed in civil, mechanical, and aerospace engineering fields. Additional topics include mixed order elements, extension to layered composite structures, and the analysis of multifield problems involving mechanical, electrical and thermal loadings.

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Produktdetails

• Verlag: Wiley & Sons
• 1. Auflage
• Seitenzahl: 410
• Erscheinungstermin: 29. September 2014
• Englisch
• Abmessung: 250mm x 175mm x 27mm
• Gewicht: 886g
• ISBN-13: 9781119941217
• ISBN-10: 1119941210
• Artikelnr.: 40452173

Autorenporträt

Erasmo Carrera is currently a full professor at the Department of Mechanical and Aerospace Engineering at Politecnico di Torino.  He is the founder and leader of the MUL2 group at the university, which has acquired a significant international reputation in the field of multilayered structures subjected to multifield loadings, see also www.mul2.com. He has introduced the Unified Formulation, or CUF (Carrera Unified Formulation), as a tool to establish a new framework in which beam, plate and shell theories can be developed for metallic and composite multilayered structures under mechanical, thermal electrical and magnetic loadings. CUF has been applied extensively to both strong and weak forms (FE and meshless solutions). Carrera has been author and co-author of about 500 papers on structural mechanics and aerospace engineering topics. Most of these works have been published in first rate international journals, as well as of two recent books published by J Wiley & Sons. Carrera's papers have had about 500 citations with h-index=34 (data taken from Scopus). Maria Cinefra is currently a research assistant at the Politecnico di Torino. Since 2010, she has worked as a teaching assistant on the "Non-linear analysis of structures", "Structures for spatial vehicles" and "Fundamentals of structural mechanics" courses. She is currently collaborating with the Department of Mathematics at Pavia University in order to develop a mixed shell finite element based on the Carrera Unified Formulation for the analysis of composite structures. She is currently working in the STEPS regional project, in collaboration with Thales Alenia Space. M. Cinefra is also working on the extension of the shell finite element, based on the CUF, to the analysis of multi-field problems. Marco Petrolo is a Post-Doc fellow at the Politecnico di Torino (Italy). He works in Professor Carrera's research group on various research topics related to the development of refined structural models of composite structures. His research activity is connected to the structural analysis of composite lifting surfaces; refined beam, plate and shell models; component-wise approaches and axiomatic/asymptotic analyses. He is author and coauthor of some 50 publications, including 2 books and 25 articles that have been published in peer-reviewed journals. Marco has recently been appointed Adjunct Professor in Fundamentals of Strength of Materials (BSc in Mechanical Engineering at the Turin Polytechnic University in Tashkent, Uzbekistan). Enrico Zappino is a Ph.D student at the Politecnico di Torino (Italy). He has worked in Professor Erasmo Carrera's research group since 2010. His research activities concern structural analysis using classical and advanced models, multi-field analysis, composite materials and FEM advanced models. He is co-author of many works that have been published in international peer-reviewed journals. Enrico was employed as a research assistant in Professor Erasmo Carrera's group from September 2010 to January 2011, where his research, in cooperation with Tales Alenia Space (TASI), was about the panel flutter phenomena of composite panels in supersonic flows.

Inhaltsangabe

Preface xiii
List of symbols and acronyms xvii
1 Introduction 1
1.1 What is in this book 1
1.2 The finite element method 2
1.2.1 Approximation of the domain 2
1.2.2 The numerical approximation 4
1.3 Calculation of the area of a surface with a complex geometry via FEM 5
1.4 Elasticity of a bar 6
1.5 Stiffness matrix of a single bar 8
1.6 Stiffness matrix of a bar via the Principle of Virtual Displacements 11
1.7 Truss structures and their automatic calculation by means of FEM 14
1.8 Example of a truss structure 17
1.8.1 Element matrices in the local reference system 18
1.8.2 Element matrices in the global reference system 18
1.8.3 Global structure stiffness matrix assembly 19
1.8.4 Application of boundary conditions and the numerical solution 20
1.9 Outline of the book contents 22
2 Fundamental equations of three-dimensional elasticity 25
2.1 Equilibrium conditions 25
2.2 Geometrical relations 27
2.3 Hooke's law 27
2.4 Displacement formulations 28
3 From 3D problems to 2D and 1D problems: theories for beams, plates and
shells 31
3.1 Typical structures 31
3.1.1 Three-dimensional structures, 3D (solids) 32
3.1.2 Two-dimensional structures, 2D (plates, shells and membranes) 32
3.1.3 One-dimensional structures, 1D (beams and bars) 33
3.2 Axiomatic method 33
3.2.1 2D case 34
3.2.2 1D Case 37
3.3 Asymptotic method 39
4 Typical FE governing equations and procedures 41
4.1 Static response analysis 41
4.2 Free vibration analysis 42
4.3 Dynamic response analysis 43
5 Introduction to the unified formulation 47
5.1 Stiffness matrix of a bar and the related fundamental nucleus 47
5.2 Fundamental nucleus for the case of a bar element with internal nodes
49
5.2.1 The case of an arbitrary defined number of nodes 53
5.3 Combination of FEM and the theory of structure approximations: a four
indices fundamental nucleus and the Carrera unified formulation 54
5.3.1 Fundamental nucleus for a 1D element with a variable axial
displacement over the cross-section 55
5.3.2 Fundamental nucleus for a 1D structure with a complete displacement
field: the case of a refined beam model 56
5.4 CUF assembly technique 58
5.5 CUF as a unique approach for one-, two- and three-dimensional
structures 59
5.6 Literature review of the CUF 60
6 The displacement approach via the Principle of Virtual Displacements and
FN for 1D, 2D and 3D elements 65
6.1 Strong form of the equilibrium equations via PVD 65
6.1.1 The two fundamental terms of the fundamental nucleus 69
6.2 Weak form of the solid model using the PVD 69
6.3 Weak form of a solid element using indicial notation 72
6.4 Fundamental nucleus for 1D, 2D and 3D problems in unique form 73
6.4.1 Three-dimensional models 74
6.4.2 Two-dimensional models 74
6.4.3 One-dimensional models 75
6.5 CUF at a glance 76
6.5.1 Choice of Ni, Nj, F and Fs 78
7 3D FEM formulation (solid elements) 81
7.1 An 8-node element using the classical matrix notation 81
7.1.1 Stiffness Matrix 83
7.1.2 Load Vector 84
7.2 Derivation of the stiffness matrix using the indicial notation 85
7.2.1 Governing equations 86
7.2.2 Finite element approximation in the CUF framework 86
7.2.3 Stiffness matrix 87
7.2.4 Mass matrix 89
7.2.5 Loading vector 90
7.3 3D numerical integration 91
7.3.1 3D Gauss-Legendre quadrature 91
7.3.2 Isoparametric formulation 92
7.3.3 Reduced integration: shear locking correction 93
7.4 Shape functions 95
8 1D models with N-order displacement field, the Taylor Expansion class
(TE) 99
8.1 Classical models and the complete linear expansion case 99
8.1.1 The Euler-Bernoulli beam model (EBBT) 101
8.1.2 The Timoshenko beam theory (TBT) 102
8.1.3 The complete linear expansion case 105
8.1.4 A finite element based on N = 1 106
8.2 EBBT, TBT and N = 1 in unified form 107
8.2.1 Unified formulation of N = 1 108
8.2.2 EBBT and TBT as particular cases of N = 1 109
8.3 Carrera unified formulation for higher-order models 110
8.3.1 N = 3 and N = 4 112
8.3.2 N-order 113
8.4 Governing equations, finite element formulation and the fundamental
nucleus 114
8.4.1 Governing equations 115
8.4.2 Finite element formulation 116
8.4.3 Stiffness matrix 117
8.4.4 Mass matrix 120
8.4.5 Loading vector 121
8.5 Locking phenomena 122
8.5.1 Poisson locking and its correction 123
8.5.2 Shear Locking 125
8.6 Numerical applications 126
8.6.1 Structural analysis of a thin-walled cylinder 128
8.6.2 Dynamic response of compact and thin-walled structures 132
9 1D models with a physical volume/surface-based geometry and pure
displacement variables, the Lagrange Expansion class (LE) 143
9.1 Physical volume/surface approach 143
9.2 Lagrange polynomials and isoparametric formulation 145
9.2.1 Lagrange polynomials 147
9.2.2 Isoparametric formulation 150
9.3 LE displacement fields and cross-section elements 153
9.3.1 Finite element formulation and fundamental nucleus 156
9.4 Cross-section multi-elements and locally refined models 159
9.5 Numerical examples 160
9.5.1 Mesh refinement and convergence analysis 160
9.5.2 Considerations on Poisson's locking 165
9.5.3 Thin-walled structures and open cross-sections 167
9.5.4 Solid-like geometrical boundary conditions 174
9.6 The Component-Wise approach for aerospace and civil engineering
applications 184
9.6.1 CW for aeronautical structures 184
9.6.2 CW for civil engineering 197
10 2D plate models with N-order displacement field, the Taylor expansion
class 201
10.1 Classical models and the complete linear expansion 201
10.1.1 Classical plate theory 203
10.1.2 First-order shear deformation theory 205
10.1.3 The complete linear expansion case 207
10.1.4 A finite element based on N = 1 207
10.2 CPT, FSDT and N = 1 model in unified form 209
10.2.1 Unified formulation of N = 1 model 209
10.2.2 CPT and FSDT as particular cases of N = 1 211
10.3 Carrera unified formulation of N-order 211
10.3.1 N = 3 and N = 4 213
10.4 Governing equations, finite element formulation and the fundamental
nucleus 213
10.4.1 Governing equations 214
10.4.2 Finite element formulation 215
10.4.3 Stiffness matrix 216
10.4.4 Mass matrix 217
10.4.5 Loading vector 218
10.4.6 Numerical integration 218
10.5 Locking phenomena 220
10.5.1 Poisson locking and its correction 220
10.5.2 Shear locking and its correction 221
10.6 Numerical Applications 226
11 2D shell models with N-order displacement field, the Taylor expansion
class 231
11.1 Geometry description 231
11.2 Classical models and unified formulation 234
11.3 Geometrical relations for cylindrical shells 235
11.4 Governing equations, finite element formulation and the fundamental
nucleus 238
11.4.1 Governing equations 238
11.4.2 Finite element formulation 238
11.5 Membrane and shear locking phenomenon 239
11.5.1 MITC9 shell element 240
11.5.2 Stiffness matrix 244
11.6 Numerical applications 247
12 2D models with physical volume/surface-based geometry and pure
displacement variables, the Lagrange Expansion class (LE) 255
12.1 Physical volume/surface approach 255
12.2 Lagrange expansion model 258
12.3 Numerical examples 259
13 Discussion on possible best beam, plate and shell diagrams 263
13.1 The Mixed Axiomatic/Asymptotic Method 263
13.2 Static analysis of beams 267
13.2.1 Influence of the loading conditions 267
13.2.2 Influence of the cross-section geometry 268
13.2.3 Reduced models vs accuracy 269
13.3 Modal analysis of beams 271
13.3.1 Influence of the cross-section geometry 271
13.3.2 Influence of the boundary conditions 276
13.4 Static analysis of plates and shells 276
13.4.1 Influence of the boundary conditions 279
13.4.2 Influence of the loading conditions 280
13.4.3 Influence of the loading and thickness 283
13.4.4 Influence of the thickness ratio on shells 287
13.5 The best theory diagram 290
14 Mixing variable kinematic models 295
14.1 Coupling variable kinematic models via shared stiffness 296
14.1.1 Application of the shared stiffness method 298
14.2 Coupling variable kinematic models via the Lagrange multiplier method
299
14.2.1 Application of the Lagrange multiplier method to variable kinematics
models 302
14.3 Coupling variable kinematic models via the Arlequin method 303
14.3.1 Application of the Arlequin method 305
15 Extension to multilayered structures 307
15.1 Multilayered structures 307
15.2 Theories on multilayered structures 311
15.2.1 C0z-requirements 312
15.2.2 Refined theories 312
15.2.3 Zig-Zag theories 313
15.2.4 Layer-Wise theories 314
15.2.5 Mixed theories 315
15.3 Unified formulation for multilayered structures 315
15.3.1 ESL models 316
15.3.2 Inclusion of Murakami's Zig-Zag function 316
15.3.3 Layer-Wise theory and Legendre expansion 317
15.3.4 Mixed models with displacement an transverse stress variables 318
15.4 Finite element formulation 319
15.4.1 Assemblage at multi-layer level 320
15.4.2 Selected results 320
15.5 Literature on CUF extended to multilayered structures 323
16 Extension to multifield problems 329
16.1 Mechanical vs field loadings 329
16.2 The need for second generation FEs for multifaced cases 330
16.3 Constitutive equations for multifield problems 331
16.4 Variational statements for multifield problems 334
16.4.1 PVD - Principle of Virtual Displacements 335
16.4.2 RMVT - Reissner Mixed Variational Theorem 338
16.5 Use of variational statements to obtained FE equations in terms of
"Fundamental Nuclei" 340
16.5.1 PVD - applications 341
16.5.2 RMVT - applications 343
16.6 Selected results 346
16.6.1 Mechanical-Electrical coupling: static analysis of an actuator plate
347
16.6.2 Mechanical-Electrical coupling: comparison between RMVT analyses 349
16.7 Literature on CUF extended to multifield problems 349
A Numerical integration 357
A.1 Gauss-Legendre quadrature 357
B CUF finite element models: programming and implementation guidelines 361
B.1 Preprocessing and input descriptions 361
B.1.1 General FE inputs 362
B.1.2 Specific CUF inputs 367
B.2 FEM code 371
B.2.1 Stiffness and mass matrix 372
B.2.2 Stiffness and mass matrix numerical examples 377
B.2.3 Constraints and reduced models 379
B.2.4 Load vector 382
B.3 Postprocessing 384
B.3.1 Stresses and strains 385
References 386