A new multiaxial high-cycle fatigue initiation life prediction model for railroad wheels is proposed in this paper. A general fatigue damage analysis methodology for complex mechanical components is developed and applied to the wheel/rail rolling contact fatigue problem. A 3-D elasto-plastic finite
Fatigue cracking of an aircraft wheel
β Scribed by B. Kosec; G. Kovacic; L. Kosec
- Publisher
- Elsevier Science
- Year
- 2002
- Tongue
- English
- Weight
- 501 KB
- Volume
- 9
- Category
- Article
- ISSN
- 1350-6307
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β¦ Synopsis
Failures of different aircraft components are revealed and examined generally by the use of non-destructive examination methods. In further explanation and interpretation of failures fractographic and metallographic methods are indispensable. The paper deals with a crack on aircraft wheel rim. The wheel was made from 2014-T6 aluminium alloy. The crack was revealed during regular control by the maintenance unit for non-destructive examination of the Slovenian air carrier Adria Airways. The crack on the rim investigated was a typical fatigue crack. It was branched, with a size lower than the critical size for fast fracture.
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