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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

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

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

    JL - Fatigue and fracture mechanics

  • OECD FORD branch

Result continuities

  • Project

  • 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

  • e-ISSN

  • 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