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Structural health monitoring of aerospace composites /
Annotation
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
London, UK :
Academic Press is an imprint of Elsevier,
[2015]
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| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Front Cover; Structural Health Monitoring of Aerospace Composites; Copyright Page; Dedication; Contents; 1 Introduction; 1.1 Preamble; 1.2 Why Aerospace Composites?; 1.3 What are Aerospace Composites?; 1.3.1 Definition of Aerospace Composites; 1.3.2 High-Performance Fibers for Aerospace Composites Applications; 1.3.3 High-Performance Matrices for Aerospace Composites Applications; 1.3.4 Advantages of Composites in Aerospace Usage; 1.3.5 Fabrication of Aerospace Composites; 1.4 Evolution of Aerospace Composites; 1.4.1 Early Advances; 1.4.2 Composite Growth in the 1960s and 1970s.
- 1.4.3 Composites Growth Since the 1980s1.5 Today's Aerospace Composites; 1.5.1 Boeing 787 Dreamliner; 1.5.2 Airbus A350 XWB; 1.6 Challenges for Aerospace Composites; 1.6.1 Concerns About the Aerospace Use of Composites; 1.6.2 The November 2001 Accident of AA Flight 587; 1.6.3 Fatigue Behavior of Composite Materials; 1.6.4 The Future of Composites in Aerospace; 1.7 About This Book; References; 2 Fundamentals of Aerospace Composite Materials; 2.1 Introduction; 2.2 Anisotropic Elasticity; 2.2.1 Basic Notations; 2.2.2 Stresses-The Stress Tensor.
- 2.2.3 Strain-Displacement Relations-The Strain Tensor2.2.4 Stress-Strain Relations; 2.2.4.1 Stiffness Tensor; Compliance Tensor; 2.2.4.2 From Tensor Notations to Voigt Matrix Notation; 2.2.4.3 Stiffness Matrix; 2.2.4.4 Compliance Matrix; 2.2.4.5 Stress-Strain Relations for an Isotropic Material; 2.2.5 Equation of Motion in Terms of Stresses; 2.2.6 Equation of Motion in Terms of Displacements; 2.3 Unidirectional Composite Properties; 2.3.1 Elastic Constants of a Unidirectional Composite; 2.3.2 Compliance Matrix of a Unidirectional Composite.
- 2.4.4 Rotated 2D Compliance Matrix2.4.5 Proof of RTR-1=T-t; 2.5 Fully 3D Elastic Properties of a Composite Layer; 2.5.1 Orthotropic Stiffness Matrix; 2.5.2 Rotated Stiffness Matrix; 2.5.3 Equations of Motion for a Monoclinic Composite Layer; 2.5.4 Rotated Compliance Matrix; 2.5.5 Note on the Use of Closed-Form Expression in the C and S matrices; 2.5.6 Proof of RTR-1=T-t in 3D; 2.6 Problems and Exercises; References; 3 Vibration of Composite Structures; 3.1 Introduction; 3.1.1 Displacements for Axial-Flexural Vibration of Composite Plates; 3.1.2 Stress Resultants.