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Aircraft structures for engineering students [[electronic resource] /] / T.H.G. Megson
| Aircraft structures for engineering students [[electronic resource] /] / T.H.G. Megson |
| Autore | Megson T. H. G (Thomas Henry Gordon) |
| Edizione | [4th ed.] |
| Pubbl/distr/stampa | Oxford ; ; Burlington, MA, : Butterworth-Heinemann, 2007 |
| Descrizione fisica | 1 online resource (825 p.) |
| Disciplina | 629.134/31 |
| Collana | Elsevier aerospace engineering series |
| Soggetto topico | Airframes |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-281-05184-5
0-08-048831-5 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Aircraft Structures for engineering students; Copyright Page; Contents; Preface; Preface to Second Edition; Preface to Third Edition; Preface to Fourth Edition; Part A: Fundamentals of Structural Analysis; Section A1 Elasticity; Chapter 1 Basic elasticity; 1.1 Stress; 1.2 Notation for forces and stresses; 1.3 Equations of equilibrium; 1.4 Plane stress; 1.5 Boundary conditions; 1.6 Determination of stresses on inclined planes; 1.7 Principal stresses; 1.8 Mohr's circle of stress; 1.9 Strain; 1.10 Compatibility equations; 1.11 Plane strain
1.12 Determination of strains on inclined planes1.13 Principal strains; 1.14 Mohr's circle of strain; 1.15 Stress-strain relationships; 1.16 Experimental measurement of surface strains; References; Problems; Chapter 2 Two-dimensional problems in elasticity; 2.1 Two-dimensional problems; 2.2 Stress functions; 2.3 Inverse and semi-inverse methods; 2.4 St. Venant's principle; 2.5 Displacements; 2.6 Bending of an end-loaded cantilever; Reference; Problems; Chapter 3 Torsion of solid sections; 3.1 Prandtl stress function solution; 3.2 St. Venant warping function solution; 3.3 The membrane analogy 3.4 Torsion of a narrow rectangular stripReferences; Problems; Section A2 Virtual Work, Energy and Matrix Methods; Chapter 4 Virtual work and energy methods; 4.1 Work; 4.2 Principle of virtual work; 4.3 Applications of the principle of virtual work; References; Problems; Chapter 5 Energy methods; 5.1 Strain energy and complementary energy; 5.2 The principle of the stationary value of the total complementary energy; 5.3 Application to deflection problems; 5.4 Application to the solution of statically indeterminate systems; 5.5 Unit load method; 5.6 Flexibility method 5.7 Total potential energy5.8 The principle of the stationary value of the total potential energy; 5.9 Principle of superposition; 5.10 The reciprocal theorem; 5.11 Temperature effects; References; Further reading; Problems; Chapter 6 Matrix methods; 6.1 Notation; 6.2 Stiffness matrix for an elastic spring; 6.3 Stiffness matrix for two elastic springs in line; 6.4 Matrix analysis of pin-jointed frameworks; 6.5 Application to statically indeterminate frameworks; 6.6 Matrix analysis of space frames; 6.7 Stiffness matrix for a uniform beam; 6.8 Finite element method for continuum structures ReferencesFurther reading; Problems; Section A3 Thin Plate Theory; Chapter 7 Bending of thin plates; 7.1 Pure bending of thin plates; 7.2 Plates subjected to bending and twisting; 7.3 Plates subjected to a distributed transverse load; 7.4 Combined bending and in-plane loading of a thin rectangular plate; 7.5 Bending of thin plates having a small initial curvature; 7.6 Energy method for the bending of thin plates; References; Problems; Section A4 Structural Instability; Chapter 8 Columns; 8.1 Euler buckling of columns; 8.2 Inelastic buckling; 8.3 Effect of initial imperfections 8.4 Stability of beams under transverse and axial loads |
| Record Nr. | UNINA-9910457708403321 |
Megson T. H. G (Thomas Henry Gordon)
|
||
| Oxford ; ; Burlington, MA, : Butterworth-Heinemann, 2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft structures for engineering students [[electronic resource] /] / T.H.G. Megson
| Aircraft structures for engineering students [[electronic resource] /] / T.H.G. Megson |
| Autore | Megson T. H. G (Thomas Henry Gordon) |
| Edizione | [4th ed.] |
| Pubbl/distr/stampa | Oxford ; ; Burlington, MA, : Butterworth-Heinemann, 2007 |
| Descrizione fisica | 1 online resource (825 p.) |
| Disciplina | 629.134/31 |
| Collana | Elsevier aerospace engineering series |
| Soggetto topico | Airframes |
| ISBN |
1-281-05184-5
0-08-048831-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Aircraft Structures for engineering students; Copyright Page; Contents; Preface; Preface to Second Edition; Preface to Third Edition; Preface to Fourth Edition; Part A: Fundamentals of Structural Analysis; Section A1 Elasticity; Chapter 1 Basic elasticity; 1.1 Stress; 1.2 Notation for forces and stresses; 1.3 Equations of equilibrium; 1.4 Plane stress; 1.5 Boundary conditions; 1.6 Determination of stresses on inclined planes; 1.7 Principal stresses; 1.8 Mohr's circle of stress; 1.9 Strain; 1.10 Compatibility equations; 1.11 Plane strain
1.12 Determination of strains on inclined planes1.13 Principal strains; 1.14 Mohr's circle of strain; 1.15 Stress-strain relationships; 1.16 Experimental measurement of surface strains; References; Problems; Chapter 2 Two-dimensional problems in elasticity; 2.1 Two-dimensional problems; 2.2 Stress functions; 2.3 Inverse and semi-inverse methods; 2.4 St. Venant's principle; 2.5 Displacements; 2.6 Bending of an end-loaded cantilever; Reference; Problems; Chapter 3 Torsion of solid sections; 3.1 Prandtl stress function solution; 3.2 St. Venant warping function solution; 3.3 The membrane analogy 3.4 Torsion of a narrow rectangular stripReferences; Problems; Section A2 Virtual Work, Energy and Matrix Methods; Chapter 4 Virtual work and energy methods; 4.1 Work; 4.2 Principle of virtual work; 4.3 Applications of the principle of virtual work; References; Problems; Chapter 5 Energy methods; 5.1 Strain energy and complementary energy; 5.2 The principle of the stationary value of the total complementary energy; 5.3 Application to deflection problems; 5.4 Application to the solution of statically indeterminate systems; 5.5 Unit load method; 5.6 Flexibility method 5.7 Total potential energy5.8 The principle of the stationary value of the total potential energy; 5.9 Principle of superposition; 5.10 The reciprocal theorem; 5.11 Temperature effects; References; Further reading; Problems; Chapter 6 Matrix methods; 6.1 Notation; 6.2 Stiffness matrix for an elastic spring; 6.3 Stiffness matrix for two elastic springs in line; 6.4 Matrix analysis of pin-jointed frameworks; 6.5 Application to statically indeterminate frameworks; 6.6 Matrix analysis of space frames; 6.7 Stiffness matrix for a uniform beam; 6.8 Finite element method for continuum structures ReferencesFurther reading; Problems; Section A3 Thin Plate Theory; Chapter 7 Bending of thin plates; 7.1 Pure bending of thin plates; 7.2 Plates subjected to bending and twisting; 7.3 Plates subjected to a distributed transverse load; 7.4 Combined bending and in-plane loading of a thin rectangular plate; 7.5 Bending of thin plates having a small initial curvature; 7.6 Energy method for the bending of thin plates; References; Problems; Section A4 Structural Instability; Chapter 8 Columns; 8.1 Euler buckling of columns; 8.2 Inelastic buckling; 8.3 Effect of initial imperfections 8.4 Stability of beams under transverse and axial loads |
| Record Nr. | UNINA-9910784459103321 |
|
Megson T. H. G (Thomas Henry Gordon)
|
||
| Oxford ; ; Burlington, MA, : Butterworth-Heinemann, 2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft structures for engineering students / / T.H.G. Megson
| Aircraft structures for engineering students / / T.H.G. Megson |
| Autore | Megson T. H. G (Thomas Henry Gordon) |
| Edizione | [4th ed.] |
| Pubbl/distr/stampa | Oxford ; ; Burlington, MA, : Butterworth-Heinemann, 2007 |
| Descrizione fisica | 1 online resource (825 p.) |
| Disciplina |
629.134/31
629.13431 |
| Collana | Elsevier aerospace engineering series |
| Soggetto topico | Airframes |
| ISBN |
1-281-05184-5
0-08-048831-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Aircraft Structures for engineering students; Copyright Page; Contents; Preface; Preface to Second Edition; Preface to Third Edition; Preface to Fourth Edition; Part A: Fundamentals of Structural Analysis; Section A1 Elasticity; Chapter 1 Basic elasticity; 1.1 Stress; 1.2 Notation for forces and stresses; 1.3 Equations of equilibrium; 1.4 Plane stress; 1.5 Boundary conditions; 1.6 Determination of stresses on inclined planes; 1.7 Principal stresses; 1.8 Mohr's circle of stress; 1.9 Strain; 1.10 Compatibility equations; 1.11 Plane strain
1.12 Determination of strains on inclined planes1.13 Principal strains; 1.14 Mohr's circle of strain; 1.15 Stress-strain relationships; 1.16 Experimental measurement of surface strains; References; Problems; Chapter 2 Two-dimensional problems in elasticity; 2.1 Two-dimensional problems; 2.2 Stress functions; 2.3 Inverse and semi-inverse methods; 2.4 St. Venant's principle; 2.5 Displacements; 2.6 Bending of an end-loaded cantilever; Reference; Problems; Chapter 3 Torsion of solid sections; 3.1 Prandtl stress function solution; 3.2 St. Venant warping function solution; 3.3 The membrane analogy 3.4 Torsion of a narrow rectangular stripReferences; Problems; Section A2 Virtual Work, Energy and Matrix Methods; Chapter 4 Virtual work and energy methods; 4.1 Work; 4.2 Principle of virtual work; 4.3 Applications of the principle of virtual work; References; Problems; Chapter 5 Energy methods; 5.1 Strain energy and complementary energy; 5.2 The principle of the stationary value of the total complementary energy; 5.3 Application to deflection problems; 5.4 Application to the solution of statically indeterminate systems; 5.5 Unit load method; 5.6 Flexibility method 5.7 Total potential energy5.8 The principle of the stationary value of the total potential energy; 5.9 Principle of superposition; 5.10 The reciprocal theorem; 5.11 Temperature effects; References; Further reading; Problems; Chapter 6 Matrix methods; 6.1 Notation; 6.2 Stiffness matrix for an elastic spring; 6.3 Stiffness matrix for two elastic springs in line; 6.4 Matrix analysis of pin-jointed frameworks; 6.5 Application to statically indeterminate frameworks; 6.6 Matrix analysis of space frames; 6.7 Stiffness matrix for a uniform beam; 6.8 Finite element method for continuum structures ReferencesFurther reading; Problems; Section A3 Thin Plate Theory; Chapter 7 Bending of thin plates; 7.1 Pure bending of thin plates; 7.2 Plates subjected to bending and twisting; 7.3 Plates subjected to a distributed transverse load; 7.4 Combined bending and in-plane loading of a thin rectangular plate; 7.5 Bending of thin plates having a small initial curvature; 7.6 Energy method for the bending of thin plates; References; Problems; Section A4 Structural Instability; Chapter 8 Columns; 8.1 Euler buckling of columns; 8.2 Inelastic buckling; 8.3 Effect of initial imperfections 8.4 Stability of beams under transverse and axial loads |
| Record Nr. | UNINA-9910823744103321 |
|
Megson T. H. G (Thomas Henry Gordon)
|
||
| Oxford ; ; Burlington, MA, : Butterworth-Heinemann, 2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Composite materials V : selected, peer reviewed papers from the 5th China Cross-Strait Conference on Composite Materials, Shanghai, China, October 22-26, 2006 / / edited by Di Zhang, Jingkun Guo, Chi Y.A. Tsao
| Composite materials V : selected, peer reviewed papers from the 5th China Cross-Strait Conference on Composite Materials, Shanghai, China, October 22-26, 2006 / / edited by Di Zhang, Jingkun Guo, Chi Y.A. Tsao |
| Pubbl/distr/stampa | Stafa-Zurich, Switzerland ; ; Enfield, New Hampshire : , : Trans Tech Publications, , [2007] |
| Descrizione fisica | 1 online resource (274 p.) |
| Disciplina |
629.134/31
629.13431 |
| Altri autori (Persone) |
ZhangDi
GuoJingkun TsaoChi Y. A |
| Collana | Key engineering materials |
| Soggetto topico | Composite materials |
| Soggetto genere / forma | Electronic books. |
| ISBN | 3-03813-133-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Composite Materials V; Acknowledgements; Committees & Preface; Table of Contents; Microstructure Characteristics of Spray-Formed and Melt-Spun Al85Nd5Ni10 and Al89La6Ni5 Bulk Hybrid Composites; High Energy Planetary Ball Milling of SiC Powders; Thermomechanical Properties of Nanosilica Reinforced PEEK Composites; Design and Experimental Investigation of Laminated Ceramic Composites with High Strength; Microstructure and Properties of Vacuum Hot-Pressing SiC/ Ti-Cu-Ni-Sn Bulk Metallic Glass Composites
Materials Characterization in Continuous Fiber-Reinforced Ceramic Composites Served in Simulating EnvironmentFabrication of Ceramic-Metal Composites by Melt Infiltration of Moso-Bamboo-Derived Porous SiC; Oxidation Behavior of Carbon Phase in 3D C/SiC Composites; Microstructure Evolution and Microwave Dielectric Properties of Multi-Phase Ba(Ti1-xMx)O3 Ceramics; Wettability and its Improvement at Al/SiC Interfaces; Novel Composite Anode Containing Tin Compounds and Carbonaceous Materials for Li-Ion Batteries Deformation and Fracture Behavior of 7039 Al Reinforced with B4C Particles at Elevated TemperatureDevelopment and Photoluminescence of ZnO-ZnS Core-Shell Nanotube and Nanorod Arrays; Fretting Wear of SiC and Ni3Al Particles Reinforced Al Alloy Matrix Composites; Characterization on Microstructure Homogeneity of θ-Al2O3 Powder Systems During Phase Transformation; Densification Mechanism of SnO2 Ceramics Doped with 5.0 mol% MnO2; Investigation of Hot-Pressed Al2O3-Cr2O3/ Cr3C2 Nanocomposite; Consolidation and Properties of Tungsten Carbide Target with Low Cobalt Content by Hot-Press Sintering Hot Workability of the Mg65Cu20Y10Ag5 Amorphous/ NanoZrO2 Composite Alloy within Supercooled Temperature RegionStructures of Ceramics/Metal and Ceramics/Ceramics Core/Shell Particles by Hybridization; Microstructure and Mechanical Properties of Nano-ZrO2 and Nano-SiO2 Particulate Reinforced AZ31-Mg Based Composites Fabricated by Friction Stir Processing; Preparation and Conductivity of TiO2-Doped Y2O3-Stabilized ZrO2 Ceramic; Determining Interface Strength of Glass-Metal Bi-Layer Laminates Using Cross-Push Method Effects of Particle Size on the Thermal Physical Properties of SiCp/Al CompositesHigh Temperature Mechanical Property of Al2O3 Coated Quartz-Fiber Reinforced Methyl Silicon Resin Composites; Preparation and Flame Ablation/Oxidation Behavior of ZrB2/SiC Ultra-High Temperature Ceramic Composites; Friction and Wear Properties of Aluminum Matrix Composites and its Application; Fabrication and Formation Mechanism of In Situ AlN and Mg2Si Particles-Reinforced Mg Matrix Composites; Prediction of the Effect of Alloying Elements on In Situ Reaction in Synthesizing (AlN+Mg2Si)/Mg Composites Thermodynamics of the Effect of Alloying Additions on In-Situ Reaction to Synthesize TiC/Mg Composites |
| Record Nr. | UNINA-9910453740103321 |
| Stafa-Zurich, Switzerland ; ; Enfield, New Hampshire : , : Trans Tech Publications, , [2007] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Composite materials V : selected, peer reviewed papers from the 5th China Cross-Strait Conference on Composite Materials, Shanghai, China, October 22-26, 2006 / / edited by Di Zhang, Jingkun Guo, Chi Y.A. Tsao
| Composite materials V : selected, peer reviewed papers from the 5th China Cross-Strait Conference on Composite Materials, Shanghai, China, October 22-26, 2006 / / edited by Di Zhang, Jingkun Guo, Chi Y.A. Tsao |
| Pubbl/distr/stampa | Stafa-Zurich, Switzerland ; ; Enfield, New Hampshire : , : Trans Tech Publications, , [2007] |
| Descrizione fisica | 1 online resource (274 p.) |
| Disciplina |
629.134/31
629.13431 |
| Altri autori (Persone) |
ZhangDi
GuoJingkun TsaoChi Y. A |
| Collana | Key engineering materials |
| Soggetto topico | Composite materials |
| ISBN | 3-03813-133-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Composite Materials V; Acknowledgements; Committees & Preface; Table of Contents; Microstructure Characteristics of Spray-Formed and Melt-Spun Al85Nd5Ni10 and Al89La6Ni5 Bulk Hybrid Composites; High Energy Planetary Ball Milling of SiC Powders; Thermomechanical Properties of Nanosilica Reinforced PEEK Composites; Design and Experimental Investigation of Laminated Ceramic Composites with High Strength; Microstructure and Properties of Vacuum Hot-Pressing SiC/ Ti-Cu-Ni-Sn Bulk Metallic Glass Composites
Materials Characterization in Continuous Fiber-Reinforced Ceramic Composites Served in Simulating EnvironmentFabrication of Ceramic-Metal Composites by Melt Infiltration of Moso-Bamboo-Derived Porous SiC; Oxidation Behavior of Carbon Phase in 3D C/SiC Composites; Microstructure Evolution and Microwave Dielectric Properties of Multi-Phase Ba(Ti1-xMx)O3 Ceramics; Wettability and its Improvement at Al/SiC Interfaces; Novel Composite Anode Containing Tin Compounds and Carbonaceous Materials for Li-Ion Batteries Deformation and Fracture Behavior of 7039 Al Reinforced with B4C Particles at Elevated TemperatureDevelopment and Photoluminescence of ZnO-ZnS Core-Shell Nanotube and Nanorod Arrays; Fretting Wear of SiC and Ni3Al Particles Reinforced Al Alloy Matrix Composites; Characterization on Microstructure Homogeneity of θ-Al2O3 Powder Systems During Phase Transformation; Densification Mechanism of SnO2 Ceramics Doped with 5.0 mol% MnO2; Investigation of Hot-Pressed Al2O3-Cr2O3/ Cr3C2 Nanocomposite; Consolidation and Properties of Tungsten Carbide Target with Low Cobalt Content by Hot-Press Sintering Hot Workability of the Mg65Cu20Y10Ag5 Amorphous/ NanoZrO2 Composite Alloy within Supercooled Temperature RegionStructures of Ceramics/Metal and Ceramics/Ceramics Core/Shell Particles by Hybridization; Microstructure and Mechanical Properties of Nano-ZrO2 and Nano-SiO2 Particulate Reinforced AZ31-Mg Based Composites Fabricated by Friction Stir Processing; Preparation and Conductivity of TiO2-Doped Y2O3-Stabilized ZrO2 Ceramic; Determining Interface Strength of Glass-Metal Bi-Layer Laminates Using Cross-Push Method Effects of Particle Size on the Thermal Physical Properties of SiCp/Al CompositesHigh Temperature Mechanical Property of Al2O3 Coated Quartz-Fiber Reinforced Methyl Silicon Resin Composites; Preparation and Flame Ablation/Oxidation Behavior of ZrB2/SiC Ultra-High Temperature Ceramic Composites; Friction and Wear Properties of Aluminum Matrix Composites and its Application; Fabrication and Formation Mechanism of In Situ AlN and Mg2Si Particles-Reinforced Mg Matrix Composites; Prediction of the Effect of Alloying Elements on In Situ Reaction in Synthesizing (AlN+Mg2Si)/Mg Composites Thermodynamics of the Effect of Alloying Additions on In-Situ Reaction to Synthesize TiC/Mg Composites |
| Record Nr. | UNINA-9910790895803321 |
| Stafa-Zurich, Switzerland ; ; Enfield, New Hampshire : , : Trans Tech Publications, , [2007] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Composite materials V : selected, peer reviewed papers from the 5th China Cross-Strait Conference on Composite Materials, Shanghai, China, October 22-26, 2006 / / edited by Di Zhang, Jingkun Guo, Chi Y.A. Tsao
| Composite materials V : selected, peer reviewed papers from the 5th China Cross-Strait Conference on Composite Materials, Shanghai, China, October 22-26, 2006 / / edited by Di Zhang, Jingkun Guo, Chi Y.A. Tsao |
| Pubbl/distr/stampa | Stafa-Zurich, Switzerland ; ; Enfield, New Hampshire : , : Trans Tech Publications, , [2007] |
| Descrizione fisica | 1 online resource (274 p.) |
| Disciplina |
629.134/31
629.13431 |
| Altri autori (Persone) |
ZhangDi
GuoJingkun TsaoChi Y. A |
| Collana | Key engineering materials |
| Soggetto topico | Composite materials |
| ISBN | 3-03813-133-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Composite Materials V; Acknowledgements; Committees & Preface; Table of Contents; Microstructure Characteristics of Spray-Formed and Melt-Spun Al85Nd5Ni10 and Al89La6Ni5 Bulk Hybrid Composites; High Energy Planetary Ball Milling of SiC Powders; Thermomechanical Properties of Nanosilica Reinforced PEEK Composites; Design and Experimental Investigation of Laminated Ceramic Composites with High Strength; Microstructure and Properties of Vacuum Hot-Pressing SiC/ Ti-Cu-Ni-Sn Bulk Metallic Glass Composites
Materials Characterization in Continuous Fiber-Reinforced Ceramic Composites Served in Simulating EnvironmentFabrication of Ceramic-Metal Composites by Melt Infiltration of Moso-Bamboo-Derived Porous SiC; Oxidation Behavior of Carbon Phase in 3D C/SiC Composites; Microstructure Evolution and Microwave Dielectric Properties of Multi-Phase Ba(Ti1-xMx)O3 Ceramics; Wettability and its Improvement at Al/SiC Interfaces; Novel Composite Anode Containing Tin Compounds and Carbonaceous Materials for Li-Ion Batteries Deformation and Fracture Behavior of 7039 Al Reinforced with B4C Particles at Elevated TemperatureDevelopment and Photoluminescence of ZnO-ZnS Core-Shell Nanotube and Nanorod Arrays; Fretting Wear of SiC and Ni3Al Particles Reinforced Al Alloy Matrix Composites; Characterization on Microstructure Homogeneity of θ-Al2O3 Powder Systems During Phase Transformation; Densification Mechanism of SnO2 Ceramics Doped with 5.0 mol% MnO2; Investigation of Hot-Pressed Al2O3-Cr2O3/ Cr3C2 Nanocomposite; Consolidation and Properties of Tungsten Carbide Target with Low Cobalt Content by Hot-Press Sintering Hot Workability of the Mg65Cu20Y10Ag5 Amorphous/ NanoZrO2 Composite Alloy within Supercooled Temperature RegionStructures of Ceramics/Metal and Ceramics/Ceramics Core/Shell Particles by Hybridization; Microstructure and Mechanical Properties of Nano-ZrO2 and Nano-SiO2 Particulate Reinforced AZ31-Mg Based Composites Fabricated by Friction Stir Processing; Preparation and Conductivity of TiO2-Doped Y2O3-Stabilized ZrO2 Ceramic; Determining Interface Strength of Glass-Metal Bi-Layer Laminates Using Cross-Push Method Effects of Particle Size on the Thermal Physical Properties of SiCp/Al CompositesHigh Temperature Mechanical Property of Al2O3 Coated Quartz-Fiber Reinforced Methyl Silicon Resin Composites; Preparation and Flame Ablation/Oxidation Behavior of ZrB2/SiC Ultra-High Temperature Ceramic Composites; Friction and Wear Properties of Aluminum Matrix Composites and its Application; Fabrication and Formation Mechanism of In Situ AlN and Mg2Si Particles-Reinforced Mg Matrix Composites; Prediction of the Effect of Alloying Elements on In Situ Reaction in Synthesizing (AlN+Mg2Si)/Mg Composites Thermodynamics of the Effect of Alloying Additions on In-Situ Reaction to Synthesize TiC/Mg Composites |
| Record Nr. | UNINA-9910820279003321 |
| Stafa-Zurich, Switzerland ; ; Enfield, New Hampshire : , : Trans Tech Publications, , [2007] | ||
| 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-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 |
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Kassapoglou Christos
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| Chichester [England], : John Wiley & Sons Inc., 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Introduction to structural dynamics and aeroelasticity / / Dewey H. Hodges, G. Alvin Pierce [[electronic resource]]
| Introduction to structural dynamics and aeroelasticity / / Dewey H. Hodges, G. Alvin Pierce [[electronic resource]] |
| Autore | Hodges Dewey H. |
| Edizione | [Second edition.] |
| Pubbl/distr/stampa | Cambridge : , : Cambridge University Press, , 2011 |
| Descrizione fisica | 1 online resource (xxi, 247 pages) : digital, PDF file(s) |
| Disciplina | 629.134/31 |
| Collana | Cambridge aerospace series |
| Soggetto topico |
Space vehicles - Dynamics
Aeroelasticity |
| ISBN |
1-107-21462-9
1-139-11939-7 1-283-29847-3 9786613298478 1-139-12296-7 0-511-99711-6 1-139-11722-X 1-139-12788-8 1-139-11069-1 1-139-11286-4 1-139-11505-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover; Title; Copyright; Contents; Figures; Tables; Foreword; From First Edition; Addendum for Second Edition; 1 Introduction; 2 Mechanics Fundamentals; 2.1 Particles and Rigid Bodies; 2.1.1 Newton's Laws; 2.1.2 Euler's Laws and Rigid Bodies; 2.1.3 Kinetic Energy; 2.1.4 Work; 2.1.5 Lagrange's Equations; 2.2 Modeling the Dynamics of Strings; 2.2.1 Equations of Motion; 2.2.2 Strain Energy; 2.2.3 Kinetic Energy; 2.2.4 Virtual Work of Applied, Distributed Force; 2.3 Elementary Beam Theory; 2.3.1 Torsion; 2.3.2 Bending; 2.4 Composite Beams
2.4.1 Constitutive Law and Strain Energy for Coupled Bending and Torsion2.4.2 Inertia Forces and Kinetic Energy for Coupled Bending and Torsion; 2.4.3 Equations of Motion for Coupled Bending and Torsion; 2.5 The Notion of Stability; 2.6 Systems with One Degree of Freedom; 2.6.1 Unforced Motion; 2.6.2 Harmonically Forced Motion; 2.7 Epilogue; Problems; 3 Structural Dynamics; 3.1 Uniform String Dynamics; 3.1.1 Standing Wave (Modal) Solution; 3.1.2 Orthogonality of Mode Shapes; 3.1.3 Using Orthogonality; 3.1.4 Traveling Wave Solution; 3.1.5 Generalized Equations of Motion 3.1.6 Generalized Force3.1.7 Example Calculations of Forced Response; 3.2 Uniform Beam Torsional Dynamics; 3.2.1 Equations of Motion; 3.2.2 Boundary Conditions; 3.2.3 Example Solutions for Mode Shapes and Frequencies; 3.2.4 Calculation of Forced Response; 3.3 Uniform Beam Bending Dynamics; 3.3.1 Equation of Motion; 3.3.2 General Solutions; 3.3.3 Boundary Conditions; 3.3.4 Example Solutions for Mode Shapes and Frequencies; 3.3.5 Calculation of Forced Response; 3.4 Free Vibration of Beams in Coupled Bending and Torsion; 3.4.1 Equations of Motion; 3.4.2 Boundary Conditions 3.5 Approximate Solution Techniques3.5.1 The Ritz Method; 3.5.2 Galerkin's Method; 3.5.3 The Finite Element Method; 3.6 Epilogue; Problems; 4 Static Aeroelasticity; 4.1 Wind-Tunnel Models; 4.1.1 Wall-Mounted Model; 4.1.2 Sting-Mounted Model; 4.1.3 Strut-Mounted Model; 4.1.4 Wall-Mounted Model for Application to Aileron Reversal; 4.2 Uniform Lifting Surface; 4.2.1 Steady-Flow Strip Theory; 4.2.2 Equilibrium Equation; 4.2.3 Torsional Divergence; 4.2.4 Airload Distribution; 4.2.5 Aileron Reversal; 4.2.6 Sweep Effects; 4.2.7 Composite Wings and Aeroelastic Tailoring; 4.3 Epilogue; Problems 5 Aeroelastic Flutter5.1 Stability Characteristics from Eigenvalue Analysis; 5.2 Aeroelastic Analysis of a Typical Section; 5.3 Classical Flutter Analysis; 5.3.1 One-Degree-of-Freedom Flutter; 5.3.2 Two-Degree-of-Freedom Flutter; 5.4 Engineering Solutions for Flutter; 5.4.1 The k Method; 5.4.2 The p-k Method; 5.5 Unsteady Aerodynamics; 5.5.1 Theodorsen's Unsteady Thin-Airfoil Theory; 5.5.2 Finite-State Unsteady Thin-Airfoil Theory of Peters et al.; 5.6 Flutter Prediction via Assumed Modes; 5.7 Flutter Boundary Characteristics; 5.8 Structural Dynamics, Aeroelasticity, and Certification 5.8.1 Ground-Vibration Tests |
| Altri titoli varianti | Introduction to Structural Dynamics & Aeroelasticity |
| Record Nr. | UNINA-9910458027903321 |
|
Hodges Dewey H.
|
||
| Cambridge : , : Cambridge University Press, , 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Introduction to structural dynamics and aeroelasticity / / Dewey H. Hodges, G. Alvin Pierce
| Introduction to structural dynamics and aeroelasticity / / Dewey H. Hodges, G. Alvin Pierce |
| Autore | Hodges Dewey H. |
| Edizione | [Second edition.] |
| Pubbl/distr/stampa | Cambridge : , : Cambridge University Press, , 2011 |
| Descrizione fisica | 1 online resource (xxi, 247 pages) : digital, PDF file(s) |
| Disciplina | 629.134/31 |
| Collana | Cambridge aerospace series |
| Soggetto topico |
Aeroelasticitat
Vehicles espacials - Dinàmica Space vehicles - Dynamics Aeroelasticity |
| ISBN |
1-139-92979-8
1-107-21462-9 1-139-11939-7 1-283-29847-3 9786613298478 1-139-12296-7 0-511-99711-6 1-139-11722-X 1-139-12788-8 1-139-11069-1 1-139-11286-4 1-139-11505-7 |
| Classificazione | TEC009000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover; Title; Copyright; Contents; Figures; Tables; Foreword; From First Edition; Addendum for Second Edition; 1 Introduction; 2 Mechanics Fundamentals; 2.1 Particles and Rigid Bodies; 2.1.1 Newton's Laws; 2.1.2 Euler's Laws and Rigid Bodies; 2.1.3 Kinetic Energy; 2.1.4 Work; 2.1.5 Lagrange's Equations; 2.2 Modeling the Dynamics of Strings; 2.2.1 Equations of Motion; 2.2.2 Strain Energy; 2.2.3 Kinetic Energy; 2.2.4 Virtual Work of Applied, Distributed Force; 2.3 Elementary Beam Theory; 2.3.1 Torsion; 2.3.2 Bending; 2.4 Composite Beams
2.4.1 Constitutive Law and Strain Energy for Coupled Bending and Torsion2.4.2 Inertia Forces and Kinetic Energy for Coupled Bending and Torsion; 2.4.3 Equations of Motion for Coupled Bending and Torsion; 2.5 The Notion of Stability; 2.6 Systems with One Degree of Freedom; 2.6.1 Unforced Motion; 2.6.2 Harmonically Forced Motion; 2.7 Epilogue; Problems; 3 Structural Dynamics; 3.1 Uniform String Dynamics; 3.1.1 Standing Wave (Modal) Solution; 3.1.2 Orthogonality of Mode Shapes; 3.1.3 Using Orthogonality; 3.1.4 Traveling Wave Solution; 3.1.5 Generalized Equations of Motion 3.1.6 Generalized Force3.1.7 Example Calculations of Forced Response; 3.2 Uniform Beam Torsional Dynamics; 3.2.1 Equations of Motion; 3.2.2 Boundary Conditions; 3.2.3 Example Solutions for Mode Shapes and Frequencies; 3.2.4 Calculation of Forced Response; 3.3 Uniform Beam Bending Dynamics; 3.3.1 Equation of Motion; 3.3.2 General Solutions; 3.3.3 Boundary Conditions; 3.3.4 Example Solutions for Mode Shapes and Frequencies; 3.3.5 Calculation of Forced Response; 3.4 Free Vibration of Beams in Coupled Bending and Torsion; 3.4.1 Equations of Motion; 3.4.2 Boundary Conditions 3.5 Approximate Solution Techniques3.5.1 The Ritz Method; 3.5.2 Galerkin's Method; 3.5.3 The Finite Element Method; 3.6 Epilogue; Problems; 4 Static Aeroelasticity; 4.1 Wind-Tunnel Models; 4.1.1 Wall-Mounted Model; 4.1.2 Sting-Mounted Model; 4.1.3 Strut-Mounted Model; 4.1.4 Wall-Mounted Model for Application to Aileron Reversal; 4.2 Uniform Lifting Surface; 4.2.1 Steady-Flow Strip Theory; 4.2.2 Equilibrium Equation; 4.2.3 Torsional Divergence; 4.2.4 Airload Distribution; 4.2.5 Aileron Reversal; 4.2.6 Sweep Effects; 4.2.7 Composite Wings and Aeroelastic Tailoring; 4.3 Epilogue; Problems 5 Aeroelastic Flutter5.1 Stability Characteristics from Eigenvalue Analysis; 5.2 Aeroelastic Analysis of a Typical Section; 5.3 Classical Flutter Analysis; 5.3.1 One-Degree-of-Freedom Flutter; 5.3.2 Two-Degree-of-Freedom Flutter; 5.4 Engineering Solutions for Flutter; 5.4.1 The k Method; 5.4.2 The p-k Method; 5.5 Unsteady Aerodynamics; 5.5.1 Theodorsen's Unsteady Thin-Airfoil Theory; 5.5.2 Finite-State Unsteady Thin-Airfoil Theory of Peters et al.; 5.6 Flutter Prediction via Assumed Modes; 5.7 Flutter Boundary Characteristics; 5.8 Structural Dynamics, Aeroelasticity, and Certification 5.8.1 Ground-Vibration Tests |
| Altri titoli varianti | Introduction to structural dynamics & aeroelasticity |
| Record Nr. | UNINA-9910781712603321 |
|
Hodges Dewey H.
|
||
| Cambridge : , : Cambridge University Press, , 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
