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Composite materials have been the most significant and pervasive revolution in structural mechanics, especially aerospace products, for the past 30 years. Attractive features of high strength-to-weight and high stiffness-to-weight ratios are compelling reasons why structural engineers take advantage of them for many future applications. In this reference, the author presents methods for the analysis of the geometry, structure and behaviour of composite structural elements under different loading conditions, with special consideration of the anisotropy and laminated structure of composite elements. The content is suitable for graduate-level students with a basic background in mechanics of composite materials and should be equally valuable to designers and researchers.
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