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Mechanics of aeronautical composite materials /
This book presents the principles of composite laminate sizing widely used for composite structures. The focus is on aeronautics in particular, including the concepts of limit loads and ultimate loads. After a brief overview of the main composite materials used in aeronautics, the basic theory of la...
| Clasificación: | Libro Electrónico |
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| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
London : Hoboken :
ISTE Ltd ; John Wiley & Sons, Inc.,
2017.
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| Colección: | Mechanical engineering and solid mechanics series.
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| Temas: | |
| Acceso en línea: | Texto completo |
| Sumario: | This book presents the principles of composite laminate sizing widely used for composite structures. The focus is on aeronautics in particular, including the concepts of limit loads and ultimate loads. After a brief overview of the main composite materials used in aeronautics, the basic theory of laminated plates and the associated rupture criteria are given. The author presents two fundamental cases of the sizing of aeronautical composite structures: the calculation of the holed structures and their subsequent multi-bolt joints, and the calculation of the buckling. The concept of damage tolerance is also explored, with a focus on its application for tolerance to impact damage. These notions are fundamental for understanding the specificities of the sizing of aeronautical composite structures. The book also contains corrected exercises for the reader to test their understanding of the different topics covered. |
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| Descripción Física: | 1 online resource : illustrations (some color) |
| Bibliografía: | Includes bibliographical references and index. |
| ISBN: | 9781119459033 1119459036 9781119459057 1119459052 9781523115617 1523115610 9781119459088 1119459087 |