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Mechanics of aeronautical composite ...

Bouvet, Christophe.

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Mechanics of aeronautical composite materials

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Mechanics of aeronautical composite materials/ Christopher Bouvet.
作者:	Bouvet, Christophe.
出版者:	London, UK :ISTE ; : 2017.,
面頁冊數:	1 online resource :ill. (some col.)
標題:	Laminated materials. -
電子資源:	https://onlinelibrary.wiley.com/doi/book/10.1002/9781119459057
ISBN:	9781119459057

Mechanics of aeronautical composite materials
Bouvet, Christophe.

Mechanics of aeronautical composite materials[electronic resource] /Christopher Bouvet. - 1st ed. - London, UK :ISTE ;2017. - 1 online resource :ill. (some col.) - Mechanical engineering and solid mechanics series. - Mechanical engineering and solid mechanics series..

Includes bibliographical references and index.

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.

ISBN: 9781119459057Subjects--Topical Terms:

735052
Laminated materials.

LC Class. No.: TA418.9.L3

Dewey Class. No.: 620.1/18

Mechanics of aeronautical composite materials
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245 1 0 $a Mechanics of aeronautical composite materials $h [electronic resource] / $c Christopher Bouvet.
250 $a 1st ed.
260 $a London, UK : $b ISTE ; $a Hoboken, NJ : $b John Wiley & Sons, $c 2017.
300 $a 1 online resource : $b ill. (some col.)
490 1 $a Mechanical engineering and solid mechanics series
504 $a Includes bibliographical references and index.
520 8 $a 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.
588 0 $a Online resource ; title from PDF title page (viewed August 30, 2017)
650 0 $a Laminated materials. $3 735052
650 0 $a Aeronautics $x Materials. $3 3319616
830 0 $a Mechanical engineering and solid mechanics series. $3 2084346
856 4 0 $u https://onlinelibrary.wiley.com/doi/book/10.1002/9781119459057