Fatigue Crack Growth Failure And Lifing Analyses For Metallic Aircraft Structures And Components

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    Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components
    By: Russell Wanhill; Simon Barter; Loris Molent
    Publisher:
    Springer
    Print ISBN: 9789402416732, 9402416730
    eText ISBN: 9789402416756, 9402416757
    Copyright year: 2019
    Format: EPUB
    Available from $ 59.99 USD
    SKU 9789402416756
    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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