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Mechanics of aeronautical solids, ma...
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Bouvet, Christophe.
Mechanics of aeronautical solids, materials and structures
紀錄類型:
書目-電子資源 : Monograph/item
正題名/作者:
Mechanics of aeronautical solids, materials and structuresChristophe Bouvet.
作者:
Bouvet, Christophe.
出版者:
London, UK :ISTE ;2017.
面頁冊數:
1 online resource.
標題:
Aerospace engineering.
電子資源:
https://onlinelibrary.wiley.com/doi/book/10.1002/9781119413684
ISBN:
9781119413684$q(electronic bk.)
Mechanics of aeronautical solids, materials and structures
Bouvet, Christophe.
Mechanics of aeronautical solids, materials and structures
[electronic resource] /Christophe Bouvet. - 1st ed. - London, UK :ISTE ;2017. - 1 online resource. - Mechanical engineering and solid mechanics series. - Mechanical engineering and solid mechanics series..
Includes bibliographical references and index.
The objective of this work on the mechanics of aeronautical solids, materials and structures is to give an overview of the principles necessary for sizing of structures in the aeronautical field. It begins by introducing the classical notions of mechanics: stress, strain, behavior law, and sizing criteria, with an emphasis on the criteria specific to aeronautics, such as limit loads and ultimate loads.Methods of resolution are then presented, and in particular the finite element method. Plasticity is also covered in order to highlight its influence on the sizing of structures, and in particular its benefits for design criteria.Finally, the physics of the two main materials of aeronautical structures, namely aluminum and composite materials, is approached in order to clarify the sizing criteria stated in the previous chapters.Exercises, with detailed corrections, then make it possible for the reader to test their understanding of the different subjects.
ISBN: 9781119413684$q(electronic bk.)Subjects--Topical Terms:
324294
Aerospace engineering.
LC Class. No.: TL545
Dewey Class. No.: 629.13252
Mechanics of aeronautical solids, materials and structures
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The objective of this work on the mechanics of aeronautical solids, materials and structures is to give an overview of the principles necessary for sizing of structures in the aeronautical field. It begins by introducing the classical notions of mechanics: stress, strain, behavior law, and sizing criteria, with an emphasis on the criteria specific to aeronautics, such as limit loads and ultimate loads.Methods of resolution are then presented, and in particular the finite element method. Plasticity is also covered in order to highlight its influence on the sizing of structures, and in particular its benefits for design criteria.Finally, the physics of the two main materials of aeronautical structures, namely aluminum and composite materials, is approached in order to clarify the sizing criteria stated in the previous chapters.Exercises, with detailed corrections, then make it possible for the reader to test their understanding of the different subjects.
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Description based on print version record.
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https://onlinelibrary.wiley.com/doi/book/10.1002/9781119413684
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