This paper addresses the problem of predicting residual fatigue life on aircraft engine blades after foreign object damage. An elastic predictive approach is described based on arrest of short cracks propagating from a notch, which is an idealisation of the damage. This approach is extended for the
โฆ LIBER โฆ
Foreign object damage on the leading edge of a thin blade
โ Scribed by Xi Chen
- Publisher
- Elsevier Science
- Year
- 2005
- Tongue
- English
- Weight
- 574 KB
- Volume
- 37
- Category
- Article
- ISSN
- 0167-6636
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