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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    Title :

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


    Contributors:


    Publication date :

    2019-01-01


    Size :

    6 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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