Electronic Resource

Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components

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Penilaian

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This book provides a concise discussion of fatigue crack growth (FCG) failure and lifing analysis methods for metallic aircraft structures and components. After a reasonably concise historical review, surveys are made of (i) the importance of fatigue for aircraft structural failures and the sources of fatigue nucleation and cracking, (ii) contemporary FCG lifing methods, and (iii) the Quantitative Fractography (QF) required for determining the actual FCG behaviour. These surveys are followed by the main part of the book, which is a discussion, using case histories, of the applicabilities of Linear Elastic Fracture Mechanics (LEFM) and non-LEFM methods for analysing service fatigue failures and full- and sub-scale test results. This discussion is derived primarily from the experiences of the Defence Science and Technology Group in Melbourne, Australia, and the Netherlands Aerospace Centre, Marknesse, the Netherlands.

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Availability

Inventory Code	Barcode	Call Number	Location	Status
1908001914	EB0002575	620.112 6 Wan f	Central Library	Available

Detail Information

Series Title

-

Call Number

620.112 6 Wan f

Publisher

Dordrecht : Springer Dordrecht., 2019

Collation

xi, 99p.:Ill

Language

English

ISBN/ISSN

978-94-024-1675-6

Classification

620.112 6

Content Type

Ebook

Media Type

-

Carrier Type

online resource

Edition

1

Subject(s)

Materials--Fatigue

Specific Detail Info

-

Statement of Responsibility

BRF

Other version/related

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