Evaluation of fatigue crack growth rates and threshold conditions in an Al 2124-T851 alloy at different load asymmetry considering microstructure orientation.
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F25797000%3A_____%2F14%3A%230000481" target="_blank" >RIV/25797000:_____/14:#0000481 - isvavai.cz</a>
Result on the web
<a href="http://www.scientific.net/KEM" target="_blank" >http://www.scientific.net/KEM</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.4028/www.scientific.net/KEM.577-578.321" target="_blank" >10.4028/www.scientific.net/KEM.577-578.321</a>
Alternative languages
Result language
angličtina
Original language name
Evaluation of fatigue crack growth rates and threshold conditions in an Al 2124-T851 alloy at different load asymmetry considering microstructure orientation.
Original language description
Results of a fairly comprehensive experimental programme aimed at evaluation of fatigue crack growth (FCG) rates in an aircraft Al 2124 alloy in T851 state, after hot rolling, solution annealing, small plastic strain and artificial ageing are presented and discussed. Measurement was performed not only in the region of stable crack growth, but also in the threshold region enabling to estimate threshold values of stress intensity factor range using method of regression analyses. FCG rates were evaluated in both L-T and T-S directions to evaluate sensitivity of FCG resistance on different microstructure orientation. Different load asymmetry conditions R = Fmin / F max were used, namely R = 0.1 and 0.6. Repeated measurements in more than one specimen at each condition enabled to evaluate reproducibility, scatter of measurement and to perform eventually probabilistic assessment. The reproducibility of measurement was particularly good for L-T orientation. In this case, threshold values were
Czech name
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Czech description
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Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JL - Fatigue and fracture mechanics
OECD FORD branch
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Result continuities
Project
<a href="/en/project/FR-TI2%2F557" target="_blank" >FR-TI2/557: Project MOSTA - Modernization Of Small Transport Aircraft to increase operation effectiveness and economy</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2014
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Key Engineering Materials
ISSN
1013-9826
e-ISSN
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Volume of the periodical
577-578
Issue of the periodical within the volume
2014
Country of publishing house
CH - SWITZERLAND
Number of pages
4
Pages from-to
321-324
UT code for WoS article
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EID of the result in the Scopus database
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