Tuttle M.E. Structural analysis of polymeric composite materials (Boca Raton, 2013). - ОГЛАВЛЕНИЕ / CONTENTS
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ОбложкаTuttle M.E. Structural analysis of polymeric composite materials. - 2nd ed. - Boca Raton: CRC/Taylor & Francis, 2013. - xvii, 650 p.: ill. - Incl. bibl. ref. - Ind.: p.647-650. - Пер. загл.: Структурный анализ полимерных композиционных материалов. - ISBN 978-1-4398-7512-4
 

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Оглавление / Contents
 
Preface ...................................................... xiii
Acknowledgments ................................................ xv
Author ....................................................... xvii

1    Introduction ............................................... 1
1.1  Basic Definitions .......................................... 1
1.2  Polymeric Materials ........................................ 5
     1.2.1  Basic Concepts ...................................... 5
     1.2.2  Addition versus Condensation Polymers ............... 7
     1.2.3  Molecular Structure ................................. 8
     1.2.4  Thermoplastic versus Thermoset Polymers ............ 10
     1.2.5  Amorphous versus Semicrystalline Thermoplastics .... 11
     1.2.6  A-, B-, and C-Staged Thermosets .................... 12
     1.2.7  The Glass Transition Temperature ................... 12
1.3  Fibrous Materials ......................................... 14
     1.3.1  Glass Fibers ....................................... 15
     1.3.2  Aramid Fibers ...................................... 16
     1.3.3  Graphite and Carbon Fibers ......................... 17
     1.3.4  Polyethylene Fibers ................................ 20
1.4  Commercially Available Forms .............................. 21
     1.4.1  Discontinuous Fibers ............................... 21
     1.4.2  Roving Spools ...................................... 22
     1.4.3  Woven Fabrics ...................................... 22
     1.4.4  Braided Fabrics .................................... 25
     1.4.5  Pre-Impregnated Products or "Prepreg" .............. 27
1.5  Manufacturing Processes ................................... 29
     1.5.1  Layup Techniques ................................... 29
     1.5.2  Autoclave Process Cycles ........................... 31
     1.5.3  Filament Winding ................................... 34
     1.5.4  Pultrusion ......................................... 35
     1.5.5  Resin Transfer Molding ............................. 37
1.6  Scope of This Book ........................................ 37
     References ................................................ 39

2    Review of Force, Stress, and Strain Tensors ............... 41
2.1  The Force Vector .......................................... 41
2.2  Transformation of a Force Vector .......................... 43
2.3  Normal Forces, Shear Forces, and Free-Body Diagrams ....... 50
2.4  Definition of Stress ...................................... 52
2.5  The Stress Tensor ......................................... 54
2.6  Transformation of the Stress Tensor ....................... 59
2.7  Principal Stresses ........................................ 67
2.8  Plane Stress .............................................. 71
2.9  Definition of Strain ...................................... 79
2.10 The Strain Tensor ......................................... 83
2.11 Transformation of the Strain Tensor ....................... 85
2.12 Principal Strains ......................................... 90
2.13 Strains within a Plane Perpendicular to a Principal
     Strain Direction .......................................... 93
2.14 Relating Strains to Displacement Fields .................. 100
2.15 Computer Programs 3DROTATE and 2DROTATE .................. 104
     Homework Problems ........................................ 105
     References ............................................... 109

3    Material Properties ...................................... 111
3.1  Material Properties of Anisotropic versus Isotropic
     Materials ................................................ 111
3.2  Material Properties That Relate Stress to Strain ......... 118
     3.2.1  Uniaxial Tests .................................... 119
     3.2.2  Pure Shear Tests .................................. 122
     3.2.3  Specialization to Orthotropic and Transversely
            Isotropic Composites .............................. 126
3.3  Material Properties Relating Temperature to Strain ....... 133
     3.3.1  Specialization to Orthotropic and Transversely
            Isotropic Composites .............................. 135
3.4  Material Properties Relating Moisture Content to Strain .. 136
     3.4.1  Specialization to Orthotropic and Transversely
            Isotropic Composites .............................. 137
3.5  Material Properties Relating Stress or Strain to
     Failure .................................................. 138
3.6  Predicting Elastic Composite Properties Based on
     Constituents: The Rule of Mixtures ....................... 141
     Homework Problems ........................................ 148
     References ............................................... 152

4    Elastic Response of Anisotropic Materials ................ 155
4.1  Strains Induced by Stress: Anisotropic Materials ......... 155
4.2  Strains Induced by Stress: Orthotropic and Transversely
     Isotropic Materials ...................................... 162
4.3  Strains Induced by a Change in Temperature or Moisture
     Content .................................................. 172
4.4  Strains Induced by Combined Effects of Stress,
     Temperature, and Moisture ................................ 173
     Homework Problems ........................................ 176

5    Unidirectional Composite Laminates Subject to Plane
     Stress ................................................... 179
5.1  Unidirectional Composites Referenced to the Principal
     Material Coordinate System ............................... 179
5.2  Unidirectional Composites Referenced to an Arbitrary
     Coordinate System ........................................ 194
5.3  Calculating Transformed Properties Using Material
     Invariants ............................................... 213
5.4  Effective Elastic Properties of a Unidirectional
     Composite Laminate ....................................... 217
5.5  Failure of Unidirectional Composites Referenced to the
     Principal Material Coordinate System ..................... 225
     5.5.1  The Maximum Stress Failure Criterion .............. 227
     5.5.2  The Tsai-Hill Failure Criterion ................... 228
     5.5.3  The Tsai-Wu Failure Criterion ..................... 229
5.6  Failure of Unidirectional Composites Referenced to an
     Arbitrary Coordinate System .............................. 233
     5.6.1  Uniaxial Stress ................................... 233
            5.6.1.1  Maximum Stress Criterion ................. 234
            5.6.1.2  Tsai-Hill Criterion ...................... 236
            5.6.1.3  Tsai-Wu Criterion ........................ 237
            5.6.1.4  Comparison ............................... 239
     5.6.2  Pure Shear Stress States .......................... 241
            5.6.2.1  Maximum Stress Criterion ................. 242
            5.6.2.2  Tsai-Hill Criterion ...................... 245
            5.6.2.3  Tsai-Wu Criterion ........................ 246
            5.6.2.4  Comparisons .............................. 247
5.7  Computer Programs UNIDIR and UNIFAIL ..................... 249
     5.7.1  Program UNIDIR .................................... 250
     5.7.2  Program UNIFAIL ................................... 251
     Homework Problems ........................................ 251
     References ............................................... 257

6    Thermomechanical Behavior of Multiangle Composite
     Laminates ................................................ 259
6.1  Definition of a "Thin Plate" and Allowable Plate
     Loadings ................................................. 259
6.2  Plate Deformations: The Kirchhoff Hypothesis ............. 264
6.3  Principal Curvatures ..................................... 269
6.4  Standard Methods of Describing Composite Laminates ....... 276
6.5  Calculating Ply Strains and Stresses ..................... 280
6.6  Classical Lamination Theory .............................. 294
     6.6.1  Constant Environmental Conditions ................. 296
     6.6.2  Including Changes in Environmental Conditions ..... 312
6.7  Simplifications due to Stacking Sequence ................. 326
     6.7.1  Symmetric Laminates ............................... 329
     6.7.2  Cross-Ply Laminates ............................... 332
     6.7.3  Balanced Laminates ................................ 334
     6.7.4  Balanced Angle-Ply Laminates ...................... 336
     6.7.5  Quasi-Isotropic Laminates ......................... 337
6.8  Summary of CLT Calculations .............................. 339
     6.8.1  A CLT Analysis When Loads Are Known ............... 340
     6.8.2  A CLT Analysis When Midplane Strains and
            Curvatures Are Known .............................. 341
6.9  Effective Properties of a Composite Laminate ............. 342
     6.9.1  Effective Properties Relating Stress to Strain .... 343
            6.9.1.1  Extensional Properties ................... 343
            6.9.1.2  Flexural Properties ...................... 348
     6.9.2  Effective Properties Relating Temperature or
            Moisture Content to Strain ........................ 350
6.10 Transformation of the ABD Matrix ......................... 355
6.11 Computer Program CLT ..................................... 361
6.12 Comparing Classical Lamination Theory and Finite-
     Element Analyses ......................................... 363
6.13 Free Edge Stresses ....................................... 375
     6.13.1  The Origins of Free Edge Stresses ................ 375
     6.13.2  Analytical and Numerical Studies of Free Edge
             Stresses ......................................... 381
     6.13.3  Typical Numerical Results ........................ 383
     Homework Problems ........................................ 387
     References ............................................... 394

7    Predicting Failure of a Multiangle Composite Laminate .... 397
7.1  Preliminary Discussion ................................... 397
7.2  Estimating Laminate Failure Strengths Using CLT .......... 401
     7.2.1  Using CLT to Predict First-Ply Failure ............ 401
     7.2.2  Predicting Last-Ply Failure ....................... 408
7.3  First-Ply Failure Envelopes .............................. 412
7.4  Computer Programs LAMFAIL and PROGDAM .................... 415
     7.4.1  Program LAMFAIL ................................... 417
     7.4.2  Program PROGDAM ................................... 418
     Homework Problems ........................................ 421
     References ............................................... 423

8    Composite Beams .......................................... 425
8.1  Preliminary Discussion ................................... 425
8.2  Comparing Classical Lamination Theory to Isotropic
     Beam Theory .............................................. 426
8.3  Types of Composite Beams Considered ...................... 432
8.4  Effective Axial Rigidity of Rectangular Composite Beams .. 437
8.5  Effective Flexural Rigidities of Rectangular Composite
     Beams .................................................... 440
     8.5.1  Effective Flexural Rigidity of Rectangular
            Composite Beams with Ply Interfaces Orthogonal
            to the Plane of Loading ........................... 440
     8.5.2  Effective Flexural Rigidity of Rectangular
            Composite Beams with Ply Interfaces Parallel to
            the Plane of Loading .............................. 443
8.6  Effective Axial and Flexural Rigidities for Thin-Walled
     Composite Beams .......................................... 449
8.7  Statically Determinate and Indeterminate Axially Loaded
     Composite Beams .......................................... 467
8.8  Statically Determinate and Indeterminate Transversely
     Loaded Composite Beams ................................... 472
8.9  Computer Program BEAM .................................... 487
     Homework Problems ........................................ 488
     References ............................................... 490

9    Stress Concentrations Near an Elliptical Hole ............ 491
9.1  Preliminary Discussion ................................... 491
9.2  Summary of the Savin Solution for an Anisotropic Plate
     with Elliptical Hole ..................................... 492
9.3  Circular Holes in Unidirectional Laminates ............... 498
9.4  Elliptical Holes with an Aspect Ratio of Three
     in Unidirectional Laminates .............................. 501
9.5  Circular Holes in Multiangle Laminates ................... 504
9.6  Computer Program HOLES ................................... 507
     Homework Problems ........................................ 507
     References ............................................... 508

10   The Governing Equations of Thin-Plate Theory ............. 509
10.1 Preliminary Discussion ................................... 509
10.2 Equations of Equilibrium for Symmetric Laminates ......... 515
     10.2.1 Equations of Equilibrium Expressed in Terms of
            Internal Stress and Moment Resultants,
            Transverse Loading, and Out-of-Plane
            Displacements ..................................... 516
     10.2.2 Equations of Equilibrium Expressed in Terms of
            the [ABD] Matrix, Transverse Loading, and
            Midplane Displacement Fields ...................... 526
10.3 Boundary Conditions ...................................... 529
     10.3.1 Geometric (Kinematic) Boundary Conditions ......... 530
     10.3.2 Static (Natural) Boundary Conditions .............. 531
     10.3.3 Combinations of Geometric and Static Boundary
            Conditions ........................................ 535
            10.3.3.1 Free Edge ................................ 537
            10.3.3.2 Simply Supported Edges ................... 538
            10.3.3.3 Clamped Edges ............................ 539
     10.4 Representing Arbitrary Transverse Loads as
          a Fourier Series .................................... 540
     References ............................................... 546

11   Some Exact Solutions for Specially Orthotropic
     Laminates ................................................ 547
11.1 Equations of Equilibrium for a Specially Orthotropic
     Laminate ................................................. 547
11.2 In-Plane Displacement Fields in Specially Orthotropic
     Laminates ................................................ 549
11.3 Specially Orthotropic Laminates Subject to Simple
     Supports of Type S1 ...................................... 553
11.4 Specially Orthotropic Laminates Subject to Simple
     Supports of Type S4 ...................................... 559
11.5 Specially Orthotropic Laminates with Two Simply
     Supported Edges of Type SI and Two Edges of Type S2 ...... 566
11.6 The Navier Solution Applied to a Specially Orthotropic
     Laminate Subject to Simple Supports of Type S4 ........... 572
11.7 Buckling of Rectangular Specially Orthotropic Laminates
     Subject to Simple Supports of Type S4 .................... 575
11.8 Thermal Buckling of Rectangular Specially Orthotropic
     Laminates Subject to Simple Supports of Type S1 .......... 585
11.9 Computer Program SPORTHO ................................. 589
     References ............................................... 590

12   Some Approximate Solutions for Symmetric Laminates ....... 591
12.1 Preliminary Discussion ................................... 591
12.2 In-Plane Displacement Fields ............................. 598
12.3 Potential Energy in a Thin Composite Plate ............... 602
     12.3.1 Evaluation of Strain Energy Component UI .......... 607
     12.3.2 Evaluation of Strain Energy Component UII ......... 608
     12.3.3 Evaluation of Strain Energy Component UIII ........ 612
     12.3.4 Evaluation of Work Done by Transverse Loads ....... 617
12.4 Symmetric Composite Laminates Subject to Simple
     Supports of Type S4 ...................................... 617
     12.4.1 Deflections due to a Uniform Transverse Load ...... 618
     12.4.2 Deflections due to a Sinusoidal Transverse Load ... 626
     12.4.3 Deflections due to a Transverse Load Distributed
            over an Interior Region ........................... 628
     12.4.4 Deflections due to a Transverse Point Load ........ 630
12.5 Buckling of Symmetric Composite Plates Subject to
     Simple Supports of Type S4 ............................... 631
12.6 Computer Program SYMM .................................... 635
     References ............................................... 635

Appendix A: Experimental Methods Used to Measure In-Plane
     Elastic Properties ....................................... 637
     References ............................................... 641

Appendix B: Tables of Beam Deflections and Slopes ............. 643
     Reference ................................................ 646

Index ......................................................... 647


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