Open Daily: 10am - 10pm | Alley door pickup 10am - 7pm 3038 Hennepin Ave Minneapolis, MN
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  • Open Daily: 10am - 10pm
    Alley-side Pickup: 10am - 7pm

    3038 Hennepin Ave Minneapolis, MN
    612-822-4611

Open Daily: 10am - 10pm | Alley-side Pickup: 10am - 7pm
3038 Hennepin Ave Minneapolis, MN
612-822-4611
Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components

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

Barter, Simon
Molent, Loris
Wanhill, R. J. H.

Paperback

Series: Springerbriefs in Applied Sciences and Technology

Technology & EngineeringPhysics

ISBN10: 9402416730
ISBN13: 9789402416732
Publisher: Springer
Published: Feb 27 2019
Pages: 99
Weight: 0.37
Height: 0.23 Width: 6.14 Depth: 9.21
Language: English

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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Wanhill, R. J. H.

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