Simulation of Operational Loading Spectrum and its Effect on Fatigue Crack Growth

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F15%3A%230001904" target="_blank" >RIV/00010669:_____/15:#0001904 - isvavai.cz</a>
Result on the web
<a href="http://www.sciencedirect.com/science/article/pii/S1877705815006037" target="_blank" >http://www.sciencedirect.com/science/article/pii/S1877705815006037</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1016/j.proeng.2015.02.005" target="_blank" >10.1016/j.proeng.2015.02.005</a>

Result language
angličtina
Original language name
Simulation of Operational Loading Spectrum and its Effect on Fatigue Crack Growth
Original language description
The paper presents analyses of crack growth rates for two different types of load sequences. The first one was the measured natural sequence of operational loads and the second one was evaluated as a blocked sequence with the same loading spectrum. Specimens from 2124-T851 aluminum alloy were made and tested. Numerical simulations of the performed tests were made using the FASTRAN retardation model implemented in the AFGROW software and the effect of the type of loading sequence was identified.
Czech name
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Czech description
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Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2015
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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