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Mechanics of Aeronautical Composite Materials

Christophe Bouvet
€172.30
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A01=Christophe Bouvet
aeronautical unidirectional
Author_Christophe Bouvet
behavior
Category=PHD
characteristics
composite
direction
eq_bestseller
eq_isMigrated=1
eq_nobargain
eq_non-fiction
eq_science
fracture
fracture criterion
given
laminated
membrane behavior
plate
ply
ud

Product details

  • ISBN 9781786301147
  • Weight: 635g
  • Dimensions: 163 x 239mm
  • Publication Date: 11 Aug 2017
  • Publisher: ISTE Ltd and John Wiley & Sons Inc
  • Publication City/Country: GB
  • Product Form: Hardback
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Description

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.
About Christophe Bouvet
Christophe Bouvet, ISAE-SUPAÉRO, France.

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