Determination of the Crack Tip Position by Digital Image Correlation during Static and Cyclic Fracture Toughness Tests of Aluminum Alloys
- Authors: Avtaev V.V.1, Yakovlev N.O.1, Erasov V.S.1, Podzhivotov N.Y.1
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Affiliations:
- All-Russia Institute of Aviation Materials
- Issue: Vol 2019, No 4 (2019)
- Pages: 458-465
- Section: Diagnostics and Mechanical Test Techniques
- URL: https://journals.rcsi.science/0036-0295/article/view/173222
- DOI: https://doi.org/10.1134/S0036029519040025
- ID: 173222
Cite item
Abstract
Aluminum alloy V-1167RDTV specimens 1 mm thick with a central crack are used to determine the position of the tip of a mode I crack from a strain field distribution during cyclic loading in the course of fatigue crack growth rate tests and during static loading in determining the force characteristics of fracture toughness. When analyzing the displacement and strain distributions at the crack tip, we proposed a technique to measure the length of a statically growing crack to determine critical stress intensity factor Kc for a mode I crack in plane-stress state.
About the authors
V. V. Avtaev
All-Russia Institute of Aviation Materials
Author for correspondence.
Email: darkee@mail.ru
Russian Federation, Moscow, 105005
N. O. Yakovlev
All-Russia Institute of Aviation Materials
Email: darkee@mail.ru
Russian Federation, Moscow, 105005
V. S. Erasov
All-Russia Institute of Aviation Materials
Email: darkee@mail.ru
Russian Federation, Moscow, 105005
N. Yu. Podzhivotov
All-Russia Institute of Aviation Materials
Email: darkee@mail.ru
Russian Federation, Moscow, 105005