Analysis of fatigue crack length during the determination of fracture toughness of the layer material Al-Ti
Abstract eng: The 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.
Contributors:
Publisher:
Institute of Theoretical and Applied Mechanics of the Cech Academy of Sciences, Prague
Conference Title:
Conference Title:
Engineering Mechanics 2018
Conference Venue:
Svratka, CZ
Conference Dates:
2018-05-14 / 2018-05-17
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
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Record created 2022-01-10, last modified 2022-01-10
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