Properties for Design of Composite Structures

Properties for Design of Composite Structures
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PROPERTIES FOR DESIGN OF COMPOSITE STRUCTURES A comprehensive guide to analytical methods and source code to predict the behavior of undamaged and damaged composite materials In Properties for Design of Composite Structures: Theory and Implementation Using Software , distinguished researcher Dr. Neil McCartney delivers a unique and insightful approach to the development of predictive methods for the properties of undamaged and damaged laminated composite materials. The book focuses on presenting compact analytical formulae for several important effective properties—including mechanical, thermal, and electrical—that can be applied to a variety of reinforcement geometries. The author introduces a compact notation that enables an explicit treatment of laminate property determination, including the out-of-plane shear properties required for three-dimensional numerical simulations of structural features using finite and boundary element analyses. There is also a detailed consideration of ply crack closure and a useful study of the interrelationships between the effective thermoelastic constants of damaged laminates. The book also offers: A thorough introduction to the principles and formulae for homogenous materials and applications, including continuum and fracture concepts for homogeneous materials A comprehensive exploration of the properties of undamaged composites, including undamaged composite materials with multiple phases and the properties of a single undamaged lamina Practical discussions of the properties of damaged composites, including matrix cracking in UD composites and damaged laminates Consideration of effects of delamination, fatigue, and environmentally induced damage In-depth examinations of derivations of key results, including the analysis of bridged cracks and stress transfer mechanics for cross-ply and general symmetric laminates Perfect for composite design engineers in all types of material-supplying industries and manufacturing companies, Properties for Design of Composite Structures: Theory and Implementation Using Software will also earn a place in the libraries of undergraduate and graduate students in engineering, aerospace, and materials departments.

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Neil McCartney. Properties for Design of Composite Structures

Properties for Design of Composite Structures. Theory and Implementation Using Software

Contents

List of Figures

List of Tables

Guide

Pages

Preface

About the Companion Website

1 Introduction

Reference

2 Fundamental Relations for Continuum Models

2.1 Introduction

2.2 Vectors

2.3 Tensors

2.3.1 Fourth-order Elasticity Tensors

2.4 Displacement and Velocity Vectors

2.5 Material Time Derivative

2.6 Continuity Equation

2.7 Equations of Motion and Equilibrium

2.8 Energy Balance Equation

2.8.1 Conservative Body Forces

2.9 Equations of State for Hydrostatic Stress States

2.9.1 Global Thermodynamic Relations

2.9.2 Local Thermodynamic Relations

2.10 Strain Tensor

2.11 Field Equations for Infinitesimal Deformations

2.12 Equilibrium Equations

2.13 Strain–Displacement Relations

2.14 Constitutive Equations for Anisotropic Linear Thermoelastic Solids

2.14.1 Isotropic Materials

2.15 Introducing Contracted Notation

2.16 Tensor Transformations

2.17 Transformations of Elastic Constants

2.17.1 Transverse Isotropic and Isotropic Solids

2.17.2 Introducing Familiar Thermoelastic Constants

2.18 Analysis of Bend Deformation

2.18.1 Geometry and Basic Equations

2.18.2 Stress and Displacement Fields

2.18.3 Some Special Cases

2.18.3.1 Four-point Bending Tests

2.18.3.2 Plane Strain Bending

References

3 Maxwell’s Far-field Methodology Applied to the Prediction of Effective Properties of Multiphase Isotropic Particulate Composites

3.1 Introduction

3.2 General Description of Maxwell’s Methodology Applied to Thermal Conductivity

3.2.1 Description of Geometry

3.2.2 Temperature Distribution for an Isolated Sphere Embedded in an Infinite Matrix

3.2.3 Maxwell’s Methodology for Estimating Conductivity

3.3 Bulk Modulus and Thermal Expansion Coefficient. 3.3.1 Spherical Particle Embedded in Infinite Matrix Subject to Pressure and Thermal Loading

3.3.2 Applying Maxwell’s Methodology to Isotropic Multiphase Particulate Composites

3.4 Shear Modulus. 3.4.1 Spherical Particle Embedded in Infinite Matrix Material Subject to Pure Shear Loading

3.4.2 Application of Maxwell’s Methodology

3.5 Summary of Results. 3.5.1 Multiphase Composites

3.5.2 Two-phase Composites

3.6 Bounds for Two-phase Isotropic Composites

3.7 Comparison of Predictions with Known Results

References

4 Maxwell’s Methodology for the Prediction of Effective Properties of Unidirectional Multiphase Fibre-reinforced Composites. Overview:

4.1 Introduction

4.2 General Description of Maxwell’s Methodology Applied to Thermal Conductivity

4.2.1 Temperature Distribution for an Isolated Fibre

4.2.2 Maxwell’s Methodology for Estimating Transverse Conductivity

4.3 The Basic Equations for Thermoelastic Analysis

4.3.1 Properties Defined from Axisymmetric Distributions

4.3.2 Solution for an Isolated Fibre Perfectly Bonded to the Matrix

4.3.3 Solution in the Absence of Fibre

4.3.4 Applying Maxwell’s Approach to Multiphase Fibre Composites

4.4 Axial Shear of Anisotropic Fibres

4.4.1 Solution for an Isolated Fibre Perfectly Bonded to the Matrix

4.4.2 Solution in the Absence of Fibre

4.4.3 Applying Maxwell’s Approach to Multiphase Fibre Composites

4.5 Transverse Shear of Multiphase Fibre Composites

4.5.1 Representation for Displacement Strain and Stress Distributions

4.5.2 Stress Field in the Absence of Fibre

4.5.3 Displacement and Stress Fields in Fibre

4.5.4 Displacement and Stress Fields in Matrix

4.5.5 Applying Maxwell’s Approach to Multiphase Fibre Composites

4.6 Other Effective Elastic Properties for Multiphase Fibre-reinforced Composites

4.7 Relationship between Two-phase and Multiphase Formulae

4.8 Summary of Results for Multiphase Composites

4.9 Results for Two-phase Fibre-reinforced Composites

4.10 Bounds for Two-phase Fibre-reinforced Composites

4.10.1 Thermal Conductivity

4.10.2 Axial Young’s Modulus

4.10.3 Axial Poisson’s Ratio

4.10.4 Transverse Bulk Modulus

4.10.5 Transverse Shear Modulus

4.10.6 Axial Shear Modulus

4.10.7 Axial Thermal Expansion

4.10.8 Transverse Thermal Expansion

4.11 Comparison of Predictions with Known Results

References

5 Reinforcement with Ellipsoidal Inclusions

5.1 Stress-Strain Relations

5.2 Theorems for Mean Strain and Mean Stress

5.2.1 Mean Strain

5.2.2 Mean Stress

5.3 Eshelby Theory for an Isolated Particle

5.4 Isolated Ellipsoidal Inclusion

5.5 Multiple Ellipsoidal Inclusions

5.6 Dilute Approximation

5.7 General Case

5.8 Walpole’s Notation

References

6 Properties of an Undamaged Single Lamina

6.1 Notation for the Properties of a Single Lamina

6.2 Lamina Stress-Strain Relations

6.3 Inverted Form of Lamina Stress-Strain Relations

6.4 Generalised Plane Stress Conditions

6.5 Generalised Plane Strain Conditions

6.6 Extending the Contracted Notation for Tensors

6.7 Thermoelastic Constants for Angled Laminae

6.8 Inverse Approach

6.9 Shear Coupling Parameters and Reduced Stress-Strain Relations

6.10 Mixed Form of Stress-Strain Relations

6.11 Special Case of 0o and 90o Plies

7 Effective Thermoelastic Properties of Undamaged Laminates. Overview:

7.1 Laminate Geometry (Symmetric Laminates)

7.2 Equilibrium Equations

7.3 Interfacial and Boundary Conditions

7.4 Displacement and Strain Distributions

7.5 Effective In-plane Properties for Laminate

7.6 Out-of-Plane Shear Properties

7.7 Combined Stress-Strain Relations

7.8 Stress-Strain Equations for Transverse Isotropic Materials

7.9 Accounting for Bend Deformation (Nonsymmetric Laminates)

7.10 A More Limited Explicit Formulation

7.10.1 The Stress Field

7.10.2 Calculation of Effective Through-thickness Strain

References

8 Energy Balance Approach to Fracture in Anisotropic Elastic Material. Overview:

8.1 Introduction

8.2 Thermodynamics for Isothermal Deformations

8.2.1 Local Energy Balance Equation Based on Helmholtz Energy

8.2.2 Local Energy Balance Equation Based on Gibbs Energy

8.3 Linear Thermoelasticity

8.4 Global Energy Balance Equations

8.5 Energy-based Global Fracture Criteria

8.6 Energy-based Local Fracture Criteria

8.7 Fracture Involving Cohesive Zones

8.8 Isolated Single Crack

8.8.1 Anisotropic Stress-Strain Relations

8.8.2 A Representation for Stress and Displacement Fields

8.8.3 Chebyshev Polynomial Expansion

8.8.4 Traction Distribution on the Crack

8.8.5 Stress and Displacement Fields around the Crack

8.8.6 Displacement Discontinuity across the Crack

8.8.7 Stress Intensity Factors

8.8.8 Integral Representations for the Solution of Matrix Crack Problems

8.8.9 Energy Balance Calculation

8.8.10 Special Case of Long Ply Cracks

8.8.11 Concluding Remarks

References

9 Ply Crack Formation in Symmetric Cross-ply Laminates

9.1 Fundamental Equations and Conditions

9.1.1 Basic Field Equations

9.1.2 Boundary and Interface Conditions

9.1.3 Generalised Plane Strain Conditions

9.2 Solution for Undamaged Laminates

9.3 Shear-lag Theory for Cross-ply Laminates

9.4 Generalised Plane Strain Theory for Cross-ply Laminates

9.4.1 Solution for Ply Cracks

9.5 Calculation of In-plane Thermoelastic Constants for Damaged Laminate

9.5.1 Approach 1

9.5.2 Approach 2

9.6 Through-thickness Properties of Damaged Laminates

9.7 Consideration of Ply Crack Closure

9.7.1 Uniaxial Loading in Axial Direction

9.7.2 Uniaxial Loading in In-plane Transverse Direction

9.7.3 Uniaxial Loading in Through-thickness Direction

9.7.4 Derivation of Important Interrelationships

9.7.5 An Alternative Derivation of Interrelations

9.7.5.1 Uniaxial Loading in Axial Direction

9.7.5.2 Uniaxial Loading in In-plane Transverse Direction

9.7.5.3 Uniaxial Loading in Through-thickness Direction

9.7.6 An Observation

9.8 Example Predictions

References

10 Theoretical Basis for a Model of Ply Cracking in General Symmetric Laminates

10.1 Introduction

10.2 Geometry and Basic Field Equations

10.3 Boundary Conditions for Uniformly Cracked Laminates

10.4 Generalised Plane Strain Conditions

10.5 Reduced Stress-Strain Relations for a Cracked Laminate

10.6 Interrelationships for Thermoelastic Constants

10.6.1 Ply Crack Closure for Constrained Uniaxial Loading in Axial Direction

10.6.2 Ply Crack Closure for Constrained Uniaxial Loading in In-plane Transverse Direction

10.6.3 Ply Crack Closure for Constrained Uniaxial Loading in Through-thickness Direction

10.6.4 Useful Independent Interrelationships

10.7 Predicting Crack Formation under Fixed Applied Stresses

10.8 Accounting for Nonuniform Cracking during Ply Crack Simulation

10.9 Progressive Ply Cracking

References

11 Ply Cracking in Cross-ply Laminates Subject to Biaxial Bending

11.1 Introduction

11.2 Geometry and Basic Equations

11.3 In-plane Transverse Loading and Bending

11.4 Interfacial and Boundary Conditions

11.5 Effective Stress-Strain Relations

11.6 Reduced Stress-Strain Relations for Constrained Triaxial Loading

11.7 Ply Crack Closure for Uniaxial Loading

11.7.1 Useful Independent Relationships

11.8 Energy for a Cracked Laminate Subject to Biaxial Bending

11.9 Predicting First Ply Cracking

11.10 Progressive Cracking

11.10.1 Ply Crack Formation during Simple Bending

11.10.2 Simple Bending with Thermal Residual Stresses

11.11 An Alternative Approximate Approach to Ply Cracking

References

12 Energy-based Delamination Theory for Biaxial Loading in the Presence of Thermal Stresses

12.1 Introduction

12.2 Geometry and Mode of Loading

12.3 Undamaged Laminates

12.4 Consideration of Crack Closure

12.5 Analysis for Unconstrained Conditions

12.5.1 Bonded Region of Laminate

12.5.2 Debonded Region of Laminate

12.5.3 Self-similar Region

12.5.4 Laminate Stress-Strain Relations

12.6 Analysis for Generalised Plane Strain Conditions

12.6.1 Bonded Region of Laminate

12.6.2 Debonded Region of Laminate

12.6.3 Self-similar Region

12.6.4 Laminate Stress-Strain Relations

12.7 Calculation of the Gibbs Energy

12.8 Calculation of Energy Release Rates for Delamination Growth

12.8.1 Unconstrained Delamination (σA, σT Fixed)

12.8.2 Generalised Plane Strain (σA, σT Fixed)

12.8.3 Constrained Delamination (εA, εT Fixed)

12.9 Results

12.10 Discussion

References

13 Energy Methods for Fatigue Damage Modelling of Laminates

13.1 Introduction

13.2 Defining Preexisting Damage

13.3 Fatigue Crack Growth Laws for Cracks in Homogeneous Anisotropic Materials

13.4 Ply Crack Instability Criteria for Monotonic Loading

13.5 Stress Intensity Factors and Energy Release Rates for Long Ply Cracks

13.6 Determination of Crack Bridging Parameters

13.7 Alternative Method of Calculating Energy Release Rates

13.8 Parameters Defining Cyclic Crack Tip Deformation

13.9 Fatigue Crack Growth Law for Ply Cracks in Cross-ply Laminates

13.10 Predicting Fatigue Damage and Property Degradation (First-order Model)

13.11 Material Properties for Example Simulations

13.12 Relationship of the Model to Experimental Data

13.13 Discussion

References

Note: Modelling reversed plasticity using the Dugdale model

14 Model of Composite Degradation Due to Environmental Damage

14.1 Introduction

14.2 Model Geometry

14.3 Basic Mechanics for the Parallel Bar Model of a Composite

14.4 Accounting for Defect Growth

14.5 Prediction of Maximum load

14.6 Prediction of Progressive Damage

14.7 Predicting the Failure Stress and Time to Failure

14.8 Predicting Residual Strength

14.9 Example Results

14.10 Conclusion

References

15 Maxwell’s Far-field Methodology Predicting Elastic Properties of Multiphase Composites Reinforced with Aligned Transversely Isotropic Spheroids

15.1 Introduction

15.2 General Description of Maxwell’s Methodology Applied to Spheroidal Inclusions

15.2.1 Description of Geometry

15.2.2 Maxwell’s Methodology for Estimating Elastic Constants

15.3 Isolated Spheroidal Inclusion

15.4 Far-field Displacement Distribution

15.5 Estimating Shear Properties

15.6 Far-field Solution for Nonshear Case

15.7 Solving for Parameters Defining Properties of the Effective Medium

15.7.1 Uniaxial Axial Loading

15.7.2 Plane-strain Equibiaxial Transverse Loading

15.7.3 Defining a Soluble Set of Nonlinear Algebraic Equations

15.8 Determination of Effective Composite Properties

15.9 Composites Reinforced with Isotropic Spherical Inclusions

15.10 Composites Reinforced with Aligned Transversely Isotropic Cylindrical Fibres

15.11 Discussion of Results

References

NOTE: This chapter is based on the publication

16 Debonding Models and Application to Fibre Fractures and Matrix Cracks

16.1 Introduction

16.2 Field Equations

16.3 Interfacial and Radial Boundary Conditions

16.4 Shear-lag Theory

16.4.1 Fibre Fractures

16.4.2 Matrix Cracks

16.5 More Accurate Stress-transfer Model

16.6 Determination of the Integration Functions

16.7 Derivation of Differential Equation for a Perfectly Bonded Interface

16.8 The Average Axial Displacement Functions

16.9 Axial Boundary Conditions

16.10 Perfectly Bonded Fibre/Matrix Interfaces

16.10.1 Fibre Fractures

16.10.2 Matrix Cracks

16.11 Frictionally Slipping Interfaces with Uniform Interfacial Shear Stress

16.11.1 A Simplified Model

16.11.2 An Improved Stress-transfer Model for Interface Debonding

16.12 Solution for a Debonded Interface with Coulomb Friction

16.13 Example Predictions for Carbon-fibre Composites

16.14 Prediction of Matrix Cracking

16.14.1 Solution of the Bridged Crack Problem

16.14.2 Special Case of Long Matrix Cracks

16.14.3 Consideration of Matrix Cracking for Perfectly Bonded Fibre/Matrix Interfaces

16.15 Conclusion

References

17 Interacting Bridged Ply Cracks in a Cross-ply Laminate

17.1 Introduction

17.2 Crack-bridging for Long Isolated Cracks in Cross-ply Laminates

17.3 Method of Solution for Isolated Bridged Cracks of Any Length

17.3.1 Special Case of Long Ply Cracks

17.4 Multiple Crack Problems

17.4.1 Stress, Displacement Fields and Stress Intensity Factors

17.4.2 A Uniform Preexisting Stress Distribution with Stress-free Cracks

17.4.2.1 Method Using Orthogonality

17.4.2.2 Collocation Method

17.4.3 An Arbitrary Preexisting Stress Distribution with Bridged Cracks

17.4.3.1 Method Using Orthogonality

17.4.3.2 Collocation Method

17.5 Numerical Results

17.5.1 Stress-free Cracks in an Isotropic Plate

17.5.2 Bridged Cracks

References

18 Theoretical Basis for a Model of Ply Cracking in General Symmetric Laminates

18.1 Introduction

18.2 Geometry and Basic Field Equations

18.3 Edge Boundary Conditions for Uniformly Cracked Laminates

18.4 Generalised Plane Strain Conditions

18.5 Solution for Undamaged Laminates

18.6 Stress and Displacement Fields for Cracked Laminates

18.7 Averaged Boundary Conditions and Stress-Strain Relations

18.8 Calculation of Thermoelastic Constants for Cracked Laminate

18.9 General Description of the Homogenisation Approach

18.9.1 Geometry and Basic Field Equations

18.9.2 Development of Homogenisation Procedure

Defining the thermoelastic constants of a damaged laminate

References

19 Stress-transfer Mechanics for Biaxial Bending

19.1 Introduction

19.2 Representation for Stress and Displacement Fields

19.2.1 The Stress Field

19.2.2 The Displacement Field

19.2.3 The Recurrence Relations

19.3 Derivation of Differential Equations

19.3.1 Averaging

19.3.2 The Integrated Moments

19.3.3 Additional Expressions Involving the Interfacial Displacements

19.3.4 Solving the Recurrence Relations

19.4 Application of the Boundary Conditions

19.5 Determination of Effective Constants for Undamaged and Damaged Laminates

References

Appendix A: Solution for Shear of Isolated Spherical Particle in an Infinite Matrix. 1. Spherical Shell Subject to Pure Shear Loading

2. Deformation and Stress Fields in a Spherical Particle

3. Deformation and Stress Fields in an Infinite Matrix

4. Isolated Spherical Particle Embedded in an Infinite Matrix

References

Appendix B: Elasticity Analysis of Two Concentric Cylinders

Separation Condition for a Sliding Interface

Appendix C: Gibbs Energy per Unit Volume for a Cracked Laminate

1. In-plane Biaxial Plus Shear Deformation

2. Bend Deformation

Appendix D: Crack Closure Conditions for Laminates

1. Crack Closure Analysis for Cross-ply Laminates (in the Presence of Bending)

2. Crack Closure Analysis for General Symmetric Laminates (in the Absence of Bending)

3. Crack Closure Analysis for Cross-ply Laminates with Delaminations but Without Bending

3.1 Uniaxial Axial Loading

3.2 Uniaxial in-plane Transverse Loading

Appendix E: Derivation of the Solution of Nonlinear Equations

Appendix F: Analysis for Transversely Isotropic Cylindrical Inclusions

Appendix G: Recurrence Relations, Differential Equations and Boundary Conditions. 1. Recurrence Relations

2. Derivation of Differential Equations

3. Calculation of the Coefficients

4. Boundary Conditions for the Differential Equations

Appendix H: Solution of Differential Equations

1. The Auxiliary/Characteristic Equation

2. Series Solution of the Differential Equations

Appendix I: Energy Balance Equation for Delamination Growth

Appendix J: Derivation of Energy-based Fracture Criterion for Bridged Cracks

Appendix K: Numerical Solution of Integral Equations for Bridged Cracks

1. Nonlinear Case

2. Linear Case

Index

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Neil McCartney

National Physical Laboratory, Teddington, Middlesex, UK

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and the thermodynamic temperature T (i.e. absolute temperature, which is always positive) is then defined by the relation

whereas the stress tensor is defined by

.....

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