以复合材料结构广泛应用于航空航天领域为背景，本书介绍了复合材料层合结构最重要的分析理论及其工程应用。针对复合材料结构力学理论面临的诸多挑战，结合作者多年来对复合材料结构力学的研究工作，从剪切变形理论、状态空间理论、逐层理论出发，重点研究了复合材料结构的断裂、损伤、多物理、多尺度和灵敏度分析等问题，并突出考虑梁、板、壳、加筋及夹芯等典型复合材料结构形式。本书注重理论方法与程序实现相结合，给出了大量数值验证算例和工程实例。
本书可作为航空航天工程、力学等专业的高年级本科生和研究生的教材，时也可作为从事复合材料结构分析、设计和优化问题工程师的参考书。

Dedication
Biography
Preface
Acronyms
1.Composite analysis overview
1.1 Introduction
1.1.1 History of composites
1.1.2 Applications of co mposites in aircrafts
1.2 Composite laminates
1.2.1 Definition and constituents
1.2.2 Plies
1.2.3 Laminates
1.3 Analysis schemes
1.3.1 Basic analysis schemes
1.3.2 Basic equations
1.3.3 Existing analysis theories
1.3.4 Challenges
1.3.5 Future developments
1.4 General Hooke's law
1.4.1 Hyperelastic materials
1.4.2 Monoclinic materials
1.4.3 Orthotropic materials
1.4.4 Isotropic materials
1.4.5 Plane stress-reduced constitutive relations
1.4.6 Transformation of material coefficients
1.5 Energy principles
1.5.1 Virtual displacement principle
1.5.2 Hamilton's principle
1.5.3 Mixed variational principles
References
2.Shear deformation theories
2.1 Introduction
2.2 Classical laminated plate theory
2.2.1 Displacement fields
2.2.2 Kinematic equation
2.2.3 Constitutive equations
2.2.4 Governing equations
2.3 First-order shear deformation theory
2.3.1 Displacement fields
……
3.State space theory
4.Layerwise theorise
5.Extended layerwise method
6.Multiphysical analysis
7.Analysis of complex composites
8.Progressive failure analysis
9.Multiscale analysis
10.Sensitivity analysis
11.Analysis codes