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THÔNG TIN TÀI LIỆU
Cấu trúc
ADVANCED MECHANICS OF COMPOSITE MATERIALS
Copyright page
Table of contents
PREFACE TO THE SECOND EDITION
Chapter 1. INTRODUCTION
1.1. Structural materials
1.2. Composite materials
1.3. References
Chapter 2. FUNDAMENTALS OF MECHANICS OF SOLIDS
2.1. Stresses
2.2. Equilibrium equations
2.3. Stress transformation
2.4. Principal stresses
2.5. Displacements and strains
2.6. Transformation of small strains
2.7. Compatibility equations
2.8. Admissible static and kinematic fields
2.9. Constitutive equations for an elastic solid
2.10. Formulations of the problem
2.11. Variational principles
2.12. Reference
Chapter 3. MECHANICS OF A UNIDIRECTIONAL PLY
3.1. Ply architecture
3.2. Fiber-matrix interaction
3.3. Micromechanics of a ply
3.4. Mechanical properties of a ply under tension, shear, and compression
3.5. Hybrid composites
3.6. Composites with high fiber fraction
3.7. Phenomenological homogeneous model of a ply
3.8. References
Chapter 4. MECHANICS OF A COMPOSITE LAYER
4.1. Isotropic layer
4.2. Unidirectional orthotropic layer
4.3. Unidirectional anisotropic layer
4.4. Orthogonally reinforced orthotropic layer
4.5. Angle-ply orthotropic layer
4.6. Fabric layers
4.7. Lattice layer
4.8. Spatially reinforced layers and bulk materials
4.9. References
Chapter 5. MECHANICS OF LAMINATES
5.1. Stiffness coefficients of a generalized anisotropic layer
5.2. Stiffness coefficients of a homogeneous layer
5.3. Stiffness coefficients of a laminate
5.4. Symmetric laminates
5.5. Engineering stiffness coefficients of orthotropic laminates
5.6. Quasi-homogeneous laminates
5.7. Quasi-isotropic laminates
5.8. Antisymmetric laminates
5.9. Sandwich structures
5.10. Coordinate of the reference plane
5.11. Stresses in laminates
5.12. Example
5.13. References
Chapter 6. FAILURE CRITERIA AND STRENGTH OF LAMINATES
6.1. Failure criteria for an elementary composite layer or ply
6.2. Practical recommendations
6.3. Examples
6.4. Allowable stresses for laminates consisting of unidirectional plies
6.5. References
Chapter 7. ENVIRONMENTAL, SPECIAL LOADING, AND MANUFACTURING EFFECTS
7.1. Temperature effects
7.2. Hygrothermal effects and aging
7.3. Time and time-dependent loading effects
7.4. Manufacturing effects
7.5. References
Chapter 8. OPTIMAL COMPOSITE STRUCTURES
8.1. Optimal fibrous structures
8.2. Composite laminates of uniform strength
8.3. Application to optimal composite structures
8.4. References
AUTHOR INDEX
SUBJECT INDEX
Nội dung
[...]... traditional models ofmechanics of materials developed for metals and other conventional materials can be used to describe their behavior This group of composites is not touched on in the book The second group ofcompositematerials that is under study here involves composites that are called ‘reinforced materials. ’ The basic components of these materials (sometimes referred to as advanced composites’)... thousands of years Correspondingly, the majority of natural materials that have emerged as a result of a prolonged evolution process can be treated as compositematerials With respect to the problems covered in this book we can classify existing compositematerials (composites) into two main groups The first group comprises composites that are known as ‘filled materials. ’ The main feature of these materials. .. unidirectional boron–aluminum composite 22 Advancedmechanicsofcompositematerials the mechanical properties of metal matrix composites are controlled by the matrix to a considerably larger extent, though the fibers still provide the major contribution to the strength and stiffness of the material The next step in the development ofcompositematerials that can be treated as matrix materials reinforced with... 14 Advancedmechanicsofcompositematerials There exists a special class of ceramic fibers for high-temperature applications composed of various combinations of silicon, carbon, nitrogen, aluminum, boron, and titanium The most commonly encountered are silicon carbide (SiC) and alumina (Al2 O3 ) fibers Silicon carbide is deposited on a tungsten or carbon core-fiber by the reaction of a gas mixture of. .. 1.25 1.24 1.35 – – – 2.5 16 Advancedmechanicsofcompositematerials the tow, namely the K-number that gives the number of fibers in the tow (e.g., 3K tow contains 3000 fibers) and the tex-number which is the mass in grams of 1000 m of the tow The tow tex-number depends not only on the number of fibers but also on the fiber diameter and density For example, AS4-6K tow consisting of 6000 AS4 carbon fibers... to apply methods of Mechanics of Solids that deal with equations derived for infinitesimal volumes of material And third, this allows us to simplify the strength and stiffness evaluation problem and to reduce it to a reasonable practical level not going into analysis of the actual mechanisms of material deformation and fracture 1.2 Compositematerials This book is devoted to compositematerials that emerged... the force F in Fig 1.1 as dW = F d Then, work corresponding to point 1 of the curve in Fig 1.2 is 1 W = Fd 0 s 1 0 e Fig 1.2 Stress–strain curve for an elastic material 4 Advancedmechanicsofcompositematerials where 1 is the elongation of the bar corresponding to point 1 of the curve The work W is equal to elastic energy of the bar which is proportional to the bar’s volume and can be presented... given data are of a broad nature and are not expected to be used in design or analysis of particular composite structures More complete description ofcompositematerials and their components including the history of development and advancement, chemical compositions, physical characteristics, manufacturing, and applications can be found elsewhere (Peters, 1998) 1.2.1 Fibers for advanced composites Continuous... strain increases under a constant force This phenomenon is called the creep of the material So, the most general material model that is used in this book can be described with a constitutive equation of the following type: ε = f (σ, t, T ) (1.9) 6 Advancedmechanicsofcompositematerials Table 1.1 Mechanical properties of structural materials and fibers Material Ultimate tensile stress, σ (MPa) Modulus,... Toughness 83 Micromechanics of a Ply 86 Mechanical Properties of a Ply under Tension, Shear, and Compression 101 Longitudinal Tension 102 Transverse Tension 106 In-Plane Shear 110 Longitudinal Compression 113 Transverse Compression 122 Hybrid Composites 123 Composites with High Fiber Fraction 127 Phenomenological Homogeneous Model of a Ply 129 References 131 Chapter 4 Mechanicsof a Composite Layer 133 . alt=""
ADVANCED MECHANICS OF COMPOSITE MATERIALS
ADVANCED MECHANICS OF
COMPOSITE MATERIALS
Valery V. Vasiliev
Distinguished Professor
Department of Mechanics. elasticity, mechanics of composite materials, design, analysis, fabrica-
tion, and application of composite structures. According to the list of books on composites
presented