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Short fatigue crack growth in an aircraft Al-alloy of a 7075 type after shot peening

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F25797000%3A_____%2F14%3A%230000473" target="_blank" >RIV/25797000:_____/14:#0000473 - isvavai.cz</a>

  • Result on the web

    <a href="http://www.journals.elsevier.com/surface-and-coatings-technology/" target="_blank" >http://www.journals.elsevier.com/surface-and-coatings-technology/</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1016/j.surfcoat.2012.06.008" target="_blank" >10.1016/j.surfcoat.2012.06.008</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Short fatigue crack growth in an aircraft Al-alloy of a 7075 type after shot peening

  • Original language description

    An effect of shot peening with two groups of parameters representing limits for practical use in service on growth of physically short fatigue cracks in a 2.4. mm thick sheet of an aircraft V-95 Al-alloy (a type of a 7075 alloy), clad with a 7072 Al-alloy (Al-Zn1) was investigated. Using the improved experimental methodology, physically short fatigue cracks of the length from 0.2. mm to more than 3. mm, most of them between 0.8 and 1.5. mm, were prepared under high cycle fatigue repeated tensile loadingof the constant nominal stress range 160. MPa, load asymmetry R. =. 0. Specimens with existing short fatigue cracks together with some specimens with no cracks were then shot peened using two different groups of parameters. Microhardness measurement andinformative measurement of residual stresses near the peened edges were carried out. Development of crack growth after shot peening were measured and compared with crack growth in specimens without shot peening. Retardation of crack grow

  • Czech name

  • Czech description

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

Result continuities

  • Project

  • Continuities

    Z - Vyzkumny zamer (s odkazem do CEZ)

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

    Surface and Coatings Technology

  • ISSN

    0257-8972

  • e-ISSN

  • Volume of the periodical

    243

  • Issue of the periodical within the volume

    březen 2014

  • Country of publishing house

    NL - THE KINGDOM OF THE NETHERLANDS

  • Number of pages

    8

  • Pages from-to

    20-27

  • UT code for WoS article

  • EID of the result in the Scopus database