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


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Fatigue crack growth failure and lifing analyses for metallic aircraft structures and components


    Contributors:


    Publication date :

    2019


    Size :

    xi, 99 Seiten


    Remarks:

    Illustrationen, Diagramme
    Literaturverzeichnis: Seite 91-99



    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik
    DDC:    629.1



    Basic Information for Aircraft FCG Failure and Lifing Analyses

    Wanhill, Russell / Barter, Simon / Molent, Loris | Springer Verlag | 2019


    Usage based lifing

    STEVENS CRAIG WESLEY / CHAN SIMON SHU KONG / WU SIYU et al. | European Patent Office | 2020

    Free access



    Usage Based Lifing

    STEVENS CRAIG WESLEY / CHAN SIMON SHU KONG / WU SIYU et al. | European Patent Office | 2018

    Free access