Design and analysis of composite structures [[electronic resource] ] : with applications to aerospace structures / / Christos Kassapoglou |
Autore | Kassapoglou Christos |
Edizione | [2nd ed.] |
Pubbl/distr/stampa | Chichester [England], : John Wiley & Sons Inc., 2013 |
Descrizione fisica | 1 online resource (424 p.) |
Disciplina |
629.134/31
629.13431 |
Collana | Aerospace series |
Soggetto topico |
Airframes - Materials
Composite construction Structural engineering |
ISBN |
1-118-53693-2
1-118-53694-0 1-118-53695-9 |
Classificazione | TEC002000 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
DESIGN AND ANALYSIS OF COMPOSITE STRUCTURES : WITH APPLICATIONS TO AEROSPACE STRUCTURES; Contents; About the Author; Series Preface; Preface to First Edition; Preface to Second Edition; 1 Applications of Advanced Composites in Aircraft Structures; References; 2 Cost of Composites: a Qualitative Discussion; 2.1 Recurring Cost; 2.2 Nonrecurring Cost; 2.3 Technology Selection; 2.4 Summary and Conclusions; Exercises; References; 3 Review of Classical Laminated Plate Theory; 3.1 Composite Materials: Definitions, Symbols and Terminology; 3.2 Constitutive Equations in Three Dimensions
3.2.1 Tensor Transformations3.3 Constitutive Equations in Two Dimensions: Plane Stress; Exercises; References; 4 Review of Laminate Strength and Failure Criteria; 4.1 Maximum Stress Failure Theory; 4.2 Maximum Strain Failure Theory; 4.3 Tsai-Hill Failure Theory; 4.4 Tsai-Wu Failure Theory; 4.5 Puck Failure Theory; 4.6 Other Failure Theories; References; 5 Composite Structural Components and Mathematical Formulation; 5.1 Overview of Composite Airframe; 5.1.1 The Structural Design Process: The Analyst's Perspective 5.1.2 Basic Design Concept and Process/Material Considerations for Aircraft Parts5.1.3 Sources of Uncertainty: Applied Loads, Usage and Material Scatter; 5.1.3.1 Knowledge of Applied Loads; 5.1.3.2 Variability in Usage; 5.1.3.3 Material Scatter; 5.1.4 Environmental Effects; 5.1.5 Effect of Damage; 5.1.6 Design Values and Allowables; 5.1.7 Additional Considerations of the Design Process; 5.2 Governing Equations; 5.2.1 Equilibrium Equations; 5.2.2 Stress-Strain Equations; 5.2.3 Strain-Displacement Equations; 5.2.4 von Karman Anisotropic Plate Equations for Large Deflections 5.3 Reductions of Governing Equations: Applications to Specific Problems5.3.1 Composite Plate under Localized In-Plane Load; 5.3.2 Composite Plate under Out-of-Plane Point Load; 5.4 Energy Methods; 5.4.1 Energy Expressions for Composite Plates; 5.4.1.1 Internal Strain Energy U; 5.4.1.2 External Work W; Exercises; References; 6 Buckling of Composite Plates; 6.1 Buckling of Rectangular Composite Plate under Biaxial Loading; 6.2 Buckling of Rectangular Composite Plate under Uniaxial Compression; 6.2.1 Uniaxial Compression, Three Sides Simply Supported, One Side Free 6.3 Buckling of Rectangular Composite Plate under Shear6.4 Buckling of Long Rectangular Composite Plates under Shear; 6.5 Buckling of Rectangular Composite Plates under Combined Loads; 6.6 Design Equations for Different Boundary Conditions and Load Combinations; Exercises; References; 7 Post-Buckling; 7.1 Post-Buckling Analysis of Composite Panels under Compression; 7.1.1 Application: Post-Buckled Panel under Compression; 7.2 Post-Buckling Analysis of Composite Plates under Shear; 7.2.1 Post-Buckling of Stiffened Composite Panels under Shear 7.2.1.1 Application: Post-Buckled Stiffened Fuselage Skin under Shear |
Record Nr. | UNINA-9910141635403321 |
Kassapoglou Christos | ||
Chichester [England], : John Wiley & Sons Inc., 2013 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Design and analysis of composite structures [[electronic resource] ] : with applications to aerospace structures / / Christos Kassapoglou |
Autore | Kassapoglou Christos |
Edizione | [2nd ed.] |
Pubbl/distr/stampa | Chichester [England], : John Wiley & Sons Inc., 2013 |
Descrizione fisica | 1 online resource (424 p.) |
Disciplina |
629.134/31
629.13431 |
Collana | Aerospace series |
Soggetto topico |
Airframes - Materials
Composite construction Structural engineering |
ISBN |
1-118-53693-2
1-118-53694-0 1-118-53695-9 |
Classificazione | TEC002000 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
DESIGN AND ANALYSIS OF COMPOSITE STRUCTURES : WITH APPLICATIONS TO AEROSPACE STRUCTURES; Contents; About the Author; Series Preface; Preface to First Edition; Preface to Second Edition; 1 Applications of Advanced Composites in Aircraft Structures; References; 2 Cost of Composites: a Qualitative Discussion; 2.1 Recurring Cost; 2.2 Nonrecurring Cost; 2.3 Technology Selection; 2.4 Summary and Conclusions; Exercises; References; 3 Review of Classical Laminated Plate Theory; 3.1 Composite Materials: Definitions, Symbols and Terminology; 3.2 Constitutive Equations in Three Dimensions
3.2.1 Tensor Transformations3.3 Constitutive Equations in Two Dimensions: Plane Stress; Exercises; References; 4 Review of Laminate Strength and Failure Criteria; 4.1 Maximum Stress Failure Theory; 4.2 Maximum Strain Failure Theory; 4.3 Tsai-Hill Failure Theory; 4.4 Tsai-Wu Failure Theory; 4.5 Puck Failure Theory; 4.6 Other Failure Theories; References; 5 Composite Structural Components and Mathematical Formulation; 5.1 Overview of Composite Airframe; 5.1.1 The Structural Design Process: The Analyst's Perspective 5.1.2 Basic Design Concept and Process/Material Considerations for Aircraft Parts5.1.3 Sources of Uncertainty: Applied Loads, Usage and Material Scatter; 5.1.3.1 Knowledge of Applied Loads; 5.1.3.2 Variability in Usage; 5.1.3.3 Material Scatter; 5.1.4 Environmental Effects; 5.1.5 Effect of Damage; 5.1.6 Design Values and Allowables; 5.1.7 Additional Considerations of the Design Process; 5.2 Governing Equations; 5.2.1 Equilibrium Equations; 5.2.2 Stress-Strain Equations; 5.2.3 Strain-Displacement Equations; 5.2.4 von Karman Anisotropic Plate Equations for Large Deflections 5.3 Reductions of Governing Equations: Applications to Specific Problems5.3.1 Composite Plate under Localized In-Plane Load; 5.3.2 Composite Plate under Out-of-Plane Point Load; 5.4 Energy Methods; 5.4.1 Energy Expressions for Composite Plates; 5.4.1.1 Internal Strain Energy U; 5.4.1.2 External Work W; Exercises; References; 6 Buckling of Composite Plates; 6.1 Buckling of Rectangular Composite Plate under Biaxial Loading; 6.2 Buckling of Rectangular Composite Plate under Uniaxial Compression; 6.2.1 Uniaxial Compression, Three Sides Simply Supported, One Side Free 6.3 Buckling of Rectangular Composite Plate under Shear6.4 Buckling of Long Rectangular Composite Plates under Shear; 6.5 Buckling of Rectangular Composite Plates under Combined Loads; 6.6 Design Equations for Different Boundary Conditions and Load Combinations; Exercises; References; 7 Post-Buckling; 7.1 Post-Buckling Analysis of Composite Panels under Compression; 7.1.1 Application: Post-Buckled Panel under Compression; 7.2 Post-Buckling Analysis of Composite Plates under Shear; 7.2.1 Post-Buckling of Stiffened Composite Panels under Shear 7.2.1.1 Application: Post-Buckled Stiffened Fuselage Skin under Shear |
Record Nr. | UNINA-9910830263503321 |
Kassapoglou Christos | ||
Chichester [England], : John Wiley & Sons Inc., 2013 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Design and analysis of composite structures : with applications to aerospace structures / / Christos Kassapoglou |
Autore | Kassapoglou Christos |
Edizione | [2nd ed.] |
Pubbl/distr/stampa | Chichester [England], : John Wiley & Sons Inc., 2013 |
Descrizione fisica | 1 online resource (424 p.) |
Disciplina | 629.134/31 |
Collana | Aerospace series |
Soggetto topico |
Airframes - Materials
Composite construction Structural engineering |
ISBN |
9781118536933
1118536932 9781118536940 1118536940 9781118536957 1118536959 |
Classificazione | TEC002000 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
DESIGN AND ANALYSIS OF COMPOSITE STRUCTURES : WITH APPLICATIONS TO AEROSPACE STRUCTURES; Contents; About the Author; Series Preface; Preface to First Edition; Preface to Second Edition; 1 Applications of Advanced Composites in Aircraft Structures; References; 2 Cost of Composites: a Qualitative Discussion; 2.1 Recurring Cost; 2.2 Nonrecurring Cost; 2.3 Technology Selection; 2.4 Summary and Conclusions; Exercises; References; 3 Review of Classical Laminated Plate Theory; 3.1 Composite Materials: Definitions, Symbols and Terminology; 3.2 Constitutive Equations in Three Dimensions
3.2.1 Tensor Transformations3.3 Constitutive Equations in Two Dimensions: Plane Stress; Exercises; References; 4 Review of Laminate Strength and Failure Criteria; 4.1 Maximum Stress Failure Theory; 4.2 Maximum Strain Failure Theory; 4.3 Tsai-Hill Failure Theory; 4.4 Tsai-Wu Failure Theory; 4.5 Puck Failure Theory; 4.6 Other Failure Theories; References; 5 Composite Structural Components and Mathematical Formulation; 5.1 Overview of Composite Airframe; 5.1.1 The Structural Design Process: The Analyst's Perspective 5.1.2 Basic Design Concept and Process/Material Considerations for Aircraft Parts5.1.3 Sources of Uncertainty: Applied Loads, Usage and Material Scatter; 5.1.3.1 Knowledge of Applied Loads; 5.1.3.2 Variability in Usage; 5.1.3.3 Material Scatter; 5.1.4 Environmental Effects; 5.1.5 Effect of Damage; 5.1.6 Design Values and Allowables; 5.1.7 Additional Considerations of the Design Process; 5.2 Governing Equations; 5.2.1 Equilibrium Equations; 5.2.2 Stress-Strain Equations; 5.2.3 Strain-Displacement Equations; 5.2.4 von Karman Anisotropic Plate Equations for Large Deflections 5.3 Reductions of Governing Equations: Applications to Specific Problems5.3.1 Composite Plate under Localized In-Plane Load; 5.3.2 Composite Plate under Out-of-Plane Point Load; 5.4 Energy Methods; 5.4.1 Energy Expressions for Composite Plates; 5.4.1.1 Internal Strain Energy U; 5.4.1.2 External Work W; Exercises; References; 6 Buckling of Composite Plates; 6.1 Buckling of Rectangular Composite Plate under Biaxial Loading; 6.2 Buckling of Rectangular Composite Plate under Uniaxial Compression; 6.2.1 Uniaxial Compression, Three Sides Simply Supported, One Side Free 6.3 Buckling of Rectangular Composite Plate under Shear6.4 Buckling of Long Rectangular Composite Plates under Shear; 6.5 Buckling of Rectangular Composite Plates under Combined Loads; 6.6 Design Equations for Different Boundary Conditions and Load Combinations; Exercises; References; 7 Post-Buckling; 7.1 Post-Buckling Analysis of Composite Panels under Compression; 7.1.1 Application: Post-Buckled Panel under Compression; 7.2 Post-Buckling Analysis of Composite Plates under Shear; 7.2.1 Post-Buckling of Stiffened Composite Panels under Shear 7.2.1.1 Application: Post-Buckled Stiffened Fuselage Skin under Shear |
Record Nr. | UNINA-9910877137203321 |
Kassapoglou Christos | ||
Chichester [England], : John Wiley & Sons Inc., 2013 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Modeling the effect of damage in composite structures : simplified approaches / / Christos Kassapoglou |
Autore | Kassapoglou Christos |
Pubbl/distr/stampa | Chichester, England : , : Wiley, , 2015 |
Descrizione fisica | 1 online resource (253 p.) |
Disciplina | 624.171 |
Collana | Aerospace Series |
Soggetto topico |
Structural analysis (Engineering)
Composite materials - Design |
ISBN |
1-119-01324-0
1-119-01323-2 1-119-01322-4 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover ""; ""Title Page ""; ""Copyright ""; ""Contents ""; ""Series Preface ""; ""Preface ""; ""Chapter 1 Damage in Composite Structures: Notch Sensitivity ""; ""1.1 Introduction ""; ""1.2 Notch Insensitivity ""; ""1.3 'Complete' Notch Sensitivity""; ""1.4 Notch Sensitivity of Composite Materials ""; ""Exercises ""
""References """"Chapter 2 Holes ""; ""2.1 Stresses around Holes ""; ""2.2 Using the Anisotropic Elasticity Solution to Predict Failure ""; ""2.3 The Role of the Damage Zone Created Near a Hole "" ""2.4 Simplified Approaches to Predict Failure in Laminates with Holes: the Whitney-Nuismer Criteria """"2.5 Other Approaches to Predict Failure of a Laminate with a Hole ""; ""2.6 Improved Whitney-Nuismer Approach "" ""2.7 Application: Finding the Stacking Sequence Which Results in Good OHT Performance """"Exercises ""; ""References ""; ""Chapter 3 Cracks ""; ""3.1 Introduction ""; ""3.2 Modelling a Crack in a Composite Laminate ""; ""3.3 Finite-Width Effects "" ""3.4 Other Approaches for Analysis of Cracks in Composites """"3.5 Matrix Cracks ""; ""Exercises ""; ""References ""; ""Chapter 4 Delaminations ""; ""4.1 Introduction ""; ""4.2 Relation to Inspection Methods and Criteria "" ""4.3 Modelling Different Structural Details in the Presence of Delaminations "" |
Record Nr. | UNINA-9910131338703321 |
Kassapoglou Christos | ||
Chichester, England : , : Wiley, , 2015 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Modeling the effect of damage in composite structures : simplified approaches / / Christos Kassapoglou |
Autore | Kassapoglou Christos |
Pubbl/distr/stampa | Chichester, England : , : Wiley, , 2015 |
Descrizione fisica | 1 online resource (253 p.) |
Disciplina | 624.171 |
Collana | Aerospace Series |
Soggetto topico |
Structural analysis (Engineering)
Composite materials - Design |
ISBN |
1-119-01324-0
1-119-01323-2 1-119-01322-4 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover ""; ""Title Page ""; ""Copyright ""; ""Contents ""; ""Series Preface ""; ""Preface ""; ""Chapter 1 Damage in Composite Structures: Notch Sensitivity ""; ""1.1 Introduction ""; ""1.2 Notch Insensitivity ""; ""1.3 'Complete' Notch Sensitivity""; ""1.4 Notch Sensitivity of Composite Materials ""; ""Exercises ""
""References """"Chapter 2 Holes ""; ""2.1 Stresses around Holes ""; ""2.2 Using the Anisotropic Elasticity Solution to Predict Failure ""; ""2.3 The Role of the Damage Zone Created Near a Hole "" ""2.4 Simplified Approaches to Predict Failure in Laminates with Holes: the Whitney-Nuismer Criteria """"2.5 Other Approaches to Predict Failure of a Laminate with a Hole ""; ""2.6 Improved Whitney-Nuismer Approach "" ""2.7 Application: Finding the Stacking Sequence Which Results in Good OHT Performance """"Exercises ""; ""References ""; ""Chapter 3 Cracks ""; ""3.1 Introduction ""; ""3.2 Modelling a Crack in a Composite Laminate ""; ""3.3 Finite-Width Effects "" ""3.4 Other Approaches for Analysis of Cracks in Composites """"3.5 Matrix Cracks ""; ""Exercises ""; ""References ""; ""Chapter 4 Delaminations ""; ""4.1 Introduction ""; ""4.2 Relation to Inspection Methods and Criteria "" ""4.3 Modelling Different Structural Details in the Presence of Delaminations "" |
Record Nr. | UNINA-9910808374403321 |
Kassapoglou Christos | ||
Chichester, England : , : Wiley, , 2015 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|