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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Wanhill, R., Barter, S., Molent, L. (2019). EBA Example Lifing Assessment (2004): F/A-18 Horizontal Stabilator Spindles. In: Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components. SpringerBriefs in Applied Sciences and Technology. Springer, Dordrecht. https://doi.org/10.1007/978-94-024-1675-6_6
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DOI: https://doi.org/10.1007/978-94-024-1675-6_6
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