Total fatigue life prediction for Ti-alloys airframe structure based on durability and damage-tolerant design concept
Author:
Publisher
Elsevier BV
Subject
Applied Mathematics,General Mathematics
Reference18 articles.
1. Titanium alloys on the F-22 fighter airframe;James;Adv Mater Process,2002
2. Predicting the total fatigue life in metals;Makkonen;Int J Fatigue,2009
3. Fatigue damage in aircraft structures, not wanted, but tolerated?;Schijve;Int J Fatigue,2009
4. The consequences of short crack closure on fatigue crack growth under variable amplitude loading;Vormwald;Fatigue Fract Eng Mater Struct,1991
5. Prediction of the behavior of small fatigue cracks;Endo;Mater Sci Eng A,2007
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