000022786 001__ 22786
000022786 005__ 20220110134527.0
000022786 04107 $$aeng
000022786 046__ $$k2018-05-14
000022786 100__ $$aKotyk, M.
000022786 24500 $$aAnalysis of fatigue crack length during the determination of fracture toughness of the layer material Al-Ti

000022786 24630 $$n24.$$pEngineering Mechanics 2018
000022786 260__ $$bInstitute of Theoretical and Applied Mechanics of the Cech Academy of Sciences, Prague
000022786 506__ $$arestricted
000022786 520__ $$2eng$$aThe article presents the results of analysis of the breakthrough of CT type compact samples. The samples were loaded to determine typical values for determining the fracture toughness. The tested material was an explosively bonded composite formed from the combination of Ti6Al4V titanium alloy and AA2519 aluminum alloy. The paper also presents the author's system allowing for the automation of the process of generating the initial fatigue crack. As a result of the tests, it was determined that the crack in the base materials of the composite is not equal.

000022786 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000022786 653__ $$afracture mechanics, J integral, crack length, crack tip opening displacement, stress intensity factor

000022786 7112_ $$aEngineering Mechanics 2018$$cSvratka, CZ$$d2018-05-14 / 2018-05-17$$gEM2018
000022786 720__ $$aKotyk, M.$$iMaćkowiak, P.$$iPłaczek, D.$$iSołtysiak, R.
000022786 8560_ $$ffischerc@itam.cas.cz
000022786 8564_ $$s2635993$$uhttps://invenio.itam.cas.cz/record/22786/files/413.pdf$$yOriginal version of the author's contribution in proceedings, page , section FRA.
000022786 962__ $$r21225
000022786 980__ $$aPAPER