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Fatigue and fracture of fibre metal ...

Alderliesten, Rene.

Fatigue and fracture of fibre metal laminates

Record Type:	Electronic resources : Monograph/item
Title/Author:	Fatigue and fracture of fibre metal laminatesby Rene Alderliesten.
Author:	Alderliesten, Rene.
Published:	Cham :Springer International Publishing :2017.
Description:	xii, 300 p. :ill. (some col.), digital ;24 cm.
Contained By:	Springer eBooks
Subject:	Metallic compositesFatigue.
Online resource:	http://dx.doi.org/10.1007/978-3-319-56227-8
ISBN:	9783319562278$q(electronic bk.)

Fatigue and fracture of fibre metal laminates
Alderliesten, Rene.

Fatigue and fracture of fibre metal laminates[electronic resource] /by Rene Alderliesten. - Cham :Springer International Publishing :2017. - xii, 300 p. :ill. (some col.), digital ;24 cm. - Solid mechanics and its applications,v.2360925-0042 ;. - Solid mechanics and its applications ;v. 152..

I Laminate concepts and properties -- 1 Introduction -- 2 Intellectual property and patents -- 3 Laminate concepts and typical properties -- II Prediction & analysis methods -- 1 Stress-train -- 2 Blunt notch strength -- 3 Bearing strength -- 4 Fatigue initiation -- 5 Static and fatigue delamination -- 6 Fatigue crack propagation -- 7 Residual strength -- III Environmental aspects -- 1 Temperature -- 2 Effect of frequency (wave form, hold time) -- 3 Acoustic fatigue.

This book contributes to the field of hybrid technology, describing the current state of knowledge concerning the hybrid material concept of laminated metallic and composite sheets for primary aeronautical structural applications. It is the only book to date on fatigue and fracture of fibre metal laminates (FMLs) The first section of the book provides a general background of the FML technology, highlighting the major FML types developed and studied over the past decades in conjunction with an overview of industrial developments based on filed patents. In turn, the second section discusses the mechanical response to quasi-static loading, together with the fracture phenomena during quasi-static and cyclic loading. To consider the durability aspects related to strength justification and certification of primary aircraft structures, the third section discusses thermal aspects related to FMLs and their mechanical response to various environmental and acoustic conditions.

ISBN: 9783319562278$q(electronic bk.)

Standard No.: 10.1007/978-3-319-56227-8doiSubjects--Topical Terms:

779740
Metallic composites
--Fatigue.

LC Class. No.: TA481.5

Dewey Class. No.: 620.166

Fatigue and fracture of fibre metal laminates
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100 1 $a Alderliesten, Rene. $3 779739
245 1 0 $a Fatigue and fracture of fibre metal laminates $h [electronic resource] / $c by Rene Alderliesten.
260 $a Cham : $b Springer International Publishing : $b Imprint: Springer, $c 2017.
300 $a xii, 300 p. : $b ill. (some col.), digital ; $c 24 cm.
490 1 $a Solid mechanics and its applications, $x 0925-0042 ; $v v.236
505 0 $a I Laminate concepts and properties -- 1 Introduction -- 2 Intellectual property and patents -- 3 Laminate concepts and typical properties -- II Prediction & analysis methods -- 1 Stress-train -- 2 Blunt notch strength -- 3 Bearing strength -- 4 Fatigue initiation -- 5 Static and fatigue delamination -- 6 Fatigue crack propagation -- 7 Residual strength -- III Environmental aspects -- 1 Temperature -- 2 Effect of frequency (wave form, hold time) -- 3 Acoustic fatigue.
520 $a This book contributes to the field of hybrid technology, describing the current state of knowledge concerning the hybrid material concept of laminated metallic and composite sheets for primary aeronautical structural applications. It is the only book to date on fatigue and fracture of fibre metal laminates (FMLs) The first section of the book provides a general background of the FML technology, highlighting the major FML types developed and studied over the past decades in conjunction with an overview of industrial developments based on filed patents. In turn, the second section discusses the mechanical response to quasi-static loading, together with the fracture phenomena during quasi-static and cyclic loading. To consider the durability aspects related to strength justification and certification of primary aircraft structures, the third section discusses thermal aspects related to FMLs and their mechanical response to various environmental and acoustic conditions.
650 0 $a Metallic composites $x Fatigue. $3 779740
650 0 $a Fibrous composites $x Fatigue. $3 646886
650 0 $a Metallic composites $x Fracture. $3 779741
650 0 $a Fibrous composites $x Fracture. $3 770191
650 1 4 $a Engineering. $3 210888
650 2 4 $a Theoretical and Applied Mechanics. $3 274501
650 2 4 $a Characterization and Evaluation of Materials. $3 273978
650 2 4 $a Aerospace Technology and Astronautics. $3 309707
710 2 $a SpringerLink (Online service) $3 273601
773 0 $t Springer eBooks
830 0 $a Solid mechanics and its applications ; $v v. 152. $3 513892
856 4 0 $u http://dx.doi.org/10.1007/978-3-319-56227-8
950 $a Engineering (Springer-11647)