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A probabilistic approach to fatigue risk assessment in aerospace components
This paper describes a new possible approach to fatigue design of aerospace components founded on probabilistic bases compared with safe life and damage tolerance that are founded on deterministic bases. A numerical tool has been introduced and explained together with the experimental activity for i...
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Published in: | Engineering fracture mechanics 2007-12, Vol.74 (18), p.2964-2970 |
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Main Authors: | , |
Format: | Article |
Language: | English |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | This paper describes a new possible approach to fatigue design of aerospace components founded on probabilistic bases compared with safe life and damage tolerance that are founded on deterministic bases.
A numerical tool has been introduced and explained together with the experimental activity for its validation analyses.
For a typical aerospace component, such as a lap-joint panel, an acceptable maximum risk level has been established and the maintenance program has been planned to ensure operating life without catastrophic failures.
The analysis has shown that this new approach introduces several benefits in fatigue design. |
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ISSN: | 0013-7944 1873-7315 |
DOI: | 10.1016/j.engfracmech.2006.04.034 |