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.
EBA Example Lifing Assessment (2004): F/A-18 Horizontal Stabilator Spindles
Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components ; 55-60
2019-01-01
6 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
LCFLF Example Lifing Assessment (2004): F/A-18 Vertical Tail Attachment Stubs
Springer Verlag | 2019
|Virtual Product Development Case Study of the T-45 Horizontal Stabilator
British Library Conference Proceedings | 1998
|