Results of proficiency test programme on fatigue crack growth in an aircraft 7175-T7351 Al-alloy with probability life assessment example
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F25797000%3A_____%2F16%3AN0000052" target="_blank" >RIV/25797000:_____/16:N0000052 - isvavai.cz</a>
Result on the web
<a href="http://www.svum.cz" target="_blank" >http://www.svum.cz</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Results of proficiency test programme on fatigue crack growth in an aircraft 7175-T7351 Al-alloy with probability life assessment example
Original language description
Existing exact knowledge on fatigue crack growth parameters and characteristics is an essential condition for an application of Damage Tolerance design philosophy in dynamically loaded structures. Measurement of fatigue crack growth (FCG) rates in an Al 7175-T7351 alloy of a particularly high homogeneity was carried out as a part of the Proficiency Test Programme organised by Exova in France. Results were evaluated in terms of parameters C and m of the Paris dependence in the stable growth region. To pass the test programme successfully, a particular attention was paid to improve and verify DCPD (direct current potential drop) method being used for the crack length measurement. The attention paid to the experimental methodology bored fruit - the results obtained were close to the average of results measured at different accredited worldwide aircraft laboratories. Additionally, the results of the FCG measurements generated by different participating laboratories were further analyzed. A distinct correlation between C and m values, so called "coupling", was found and demonstrated. Some paradoxes of the assessment of laboratories were addressed, namely the fact that a laboratory assessed as unacceptable concerning one of the parameters generated much more accurate and useful data than another laboratory with a better assessment. Eventually, the results including their scatter were used to provide an example of probabilistic assessment of a simple beam residual life to show practical actual impacts of the scatter on the life assessment.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JL - Fatigue and fracture mechanics
OECD FORD branch
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Result continuities
Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2016
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
METAL 2016: 25th Anniversary International Conference on Metallurgy and Materials
ISBN
978-80-87294-67-3
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
1222-1227
Publisher name
TANGER Ltd
Place of publication
Ostrava
Event location
Brno
Event date
Jun 25, 2016
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
000391251200199