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Composite structures, design, safety, and innovation [e-book] / B.F. Backman
| Composite structures, design, safety, and innovation [e-book] / B.F. Backman |
| Autore | Backman, Bjorn F. |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Amsterdam ; Boston, Mass. : Elsevier, 2005 |
| Descrizione fisica | x, 244 p. : ill. ; 25 cm |
| Disciplina | 629.13431 |
| Soggetto topico |
Airframes - Materials
Composite materials Airframes - Design and construction |
| Soggetto genere / forma | Electronic books. |
| ISBN |
9780080445458
0080445454 |
| Formato | Risorse elettroniche  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | 1.0Introduction -- 2.0Structural Design -- 3.0Structural Safety -- 4.0Innovation -- 5.0Safety Objectives -- 6.0Risk Management -- 7.0Trades -- 8.0Building Block Approach -- 9.0Design Scenarios -- 10.0The Design Process -- 11.0Damage and Detection -- 12.0Design Philosophy -- 13.0Analysis of Design Criteria -- 14.0Design Example -- 15.0Design of Composite Structure -- Appendix AA Model of Ultimate Integrity -- Appendix BA Comparison between Metal and Composite Panels |
| Record Nr. | UNISALENTO-991003228409707536 |
Backman, Bjorn F.
|
||
| Amsterdam ; Boston, Mass. : Elsevier, 2005 | ||
| Risorse elettroniche | ||
| Lo trovi qui: Univ. del Salento | ||
| ||
Design and analysis of composite structures [[electronic resource] ] : with applications to aerospace structures / / Christos Kassapoglou
| 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
| 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
| 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-9911019433303321 |
|
Kassapoglou Christos
|
||
| Chichester [England], : John Wiley & Sons Inc., 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Hybrid anisotropic materials for structural aviation parts / / Yosif Golfman
| Hybrid anisotropic materials for structural aviation parts / / Yosif Golfman |
| Autore | Golfman Yosif |
| Pubbl/distr/stampa | Boca Raton : , : CRC Press, , 2011 |
| Descrizione fisica | 1 online resource (338 p.) |
| Disciplina | 629.134/3 |
| Soggetto topico |
Airframes - Materials
Composite materials Anisotropy |
| Soggetto genere / forma | Electronic books. |
| ISBN |
0-429-10620-3
1-62870-934-0 1-4398-3681-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Front cover; Contents; Preface; Acknowledgments; Chapter 1. Nanocomposite Automation Process; Chapter 2. Impregnation Process; Chapter 3. Strength Criteria and Dynamic Stability; Chapter 4. Interlaminar Shear Stress Analysis; Chapter 5. Fatigue Strength, Stress, and Vibration Analysis; Chapter 6. NDE Methods Control Properties; Chapter 7. Protective Coating Process for Aviation Parts; Back cover |
| Record Nr. | UNINA-9910459502703321 |
|
Golfman Yosif
|
||
| Boca Raton : , : CRC Press, , 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Hybrid anisotropic materials for structural aviation parts / / Yosif Golfman
| Hybrid anisotropic materials for structural aviation parts / / Yosif Golfman |
| Autore | Golfman Yosif |
| Pubbl/distr/stampa | Boca Raton : , : CRC Press, , 2011 |
| Descrizione fisica | 1 online resource (338 p.) |
| Disciplina | 629.134/3 |
| Soggetto topico |
Airframes - Materials
Composite materials Anisotropy |
| ISBN |
0-429-10620-3
1-62870-934-0 1-4398-3681-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Front cover; Contents; Preface; Acknowledgments; Chapter 1. Nanocomposite Automation Process; Chapter 2. Impregnation Process; Chapter 3. Strength Criteria and Dynamic Stability; Chapter 4. Interlaminar Shear Stress Analysis; Chapter 5. Fatigue Strength, Stress, and Vibration Analysis; Chapter 6. NDE Methods Control Properties; Chapter 7. Protective Coating Process for Aviation Parts; Back cover |
| Record Nr. | UNINA-9910785316203321 |
|
Golfman Yosif
|
||
| Boca Raton : , : CRC Press, , 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Hybrid anisotropic materials for structural aviation parts / / Yosif Golfman
| Hybrid anisotropic materials for structural aviation parts / / Yosif Golfman |
| Autore | Golfman Yosif |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Boca Raton, FL, : CRC Press, 2010 |
| Descrizione fisica | 1 online resource (338 p.) |
| Disciplina | 629.134/3 |
| Soggetto topico |
Airframes - Materials
Composite materials Anisotropy |
| ISBN |
1-04-019784-1
0-429-10620-3 1-62870-934-0 1-4398-3681-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Front cover; Contents; Preface; Acknowledgments; Chapter 1. Nanocomposite Automation Process; Chapter 2. Impregnation Process; Chapter 3. Strength Criteria and Dynamic Stability; Chapter 4. Interlaminar Shear Stress Analysis; Chapter 5. Fatigue Strength, Stress, and Vibration Analysis; Chapter 6. NDE Methods Control Properties; Chapter 7. Protective Coating Process for Aviation Parts; Back cover |
| Record Nr. | UNINA-9910968859703321 |
|
Golfman Yosif
|
||
| Boca Raton, FL, : CRC Press, 2010 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Hybrid anisotropic materials for structural aviation parts / by Yosif Golfman
| Hybrid anisotropic materials for structural aviation parts / by Yosif Golfman |
| Autore | Golfman, Yosif |
| Pubbl/distr/stampa | Boca Raton : CRC Press, 2011 |
| Descrizione fisica | xiv, 323 p. : ill. ; 24cm |
| Disciplina | 629.134/3 |
| Soggetto topico |
Airframes - Materials
Composite materials Anisotropy |
| ISBN | 9781439836804 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISALENTO-991001979349707536 |
|
Golfman, Yosif
|
||
| Boca Raton : CRC Press, 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. del Salento | ||
| ||
Impact tests for woods / / by Bureau of Standards
| Impact tests for woods / / by Bureau of Standards |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1922 |
| Descrizione fisica | 1 online resource (17 pages, 4 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Design and construction
Airframes - Materials Wood - Testing Impact - Testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713081203321 |
| [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1922 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
