Abstract As discussed in Chap. 1, Sect. 1.2.4, the EBA is a framework for predicting the FCG lives of in-service aircraft structures subjected to relatively short and repeated blocks of VA loading sequences, i.e. load sequences representative for tactical aircraft.


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    Titel :

    EBA Example Lifing Assessment (2004): F/A-18 Horizontal Stabilator Spindles


    Beteiligte:
    Wanhill, Russell (Autor:in) / Barter, Simon (Autor:in) / Molent, Loris (Autor:in)


    Erscheinungsdatum :

    2019-01-01


    Format / Umfang :

    6 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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