Fatigue crack growth in 2017A-T4 alloy subjected to proportional bending with torsion

The paper presents the results of tests on the fatigue crack growth for a constant moment amplitude under combined bending with torsion in the aluminium alloy AW-2017A-T4. The tests were performed under different values of the load ratio R. Plane specimens with stress concentrators in form of the ex...

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Main Authors: D. Rozumek, S. Faszynka
Format: Article
Language:English
Published: Gruppo Italiano Frattura 2017-09-01
Series:Fracture and Structural Integrity
Subjects:
Online Access:https://www.fracturae.com/index.php/fis/article/view/1923
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author D. Rozumek
S. Faszynka
author_facet D. Rozumek
S. Faszynka
author_sort D. Rozumek
collection DOAJ
description The paper presents the results of tests on the fatigue crack growth for a constant moment amplitude under combined bending with torsion in the aluminium alloy AW-2017A-T4. The tests were performed under different values of the load ratio R. Plane specimens with stress concentrators in form of the external one-sided sharp notch were tested. A non-uniform fatigue cracks growth on both lateral surfaces of specimens was observed during experimental tests. Fatigue cracks were developing in the specimens in two stages; quarter-elliptic edge cracks were observed at the beginning, then evolving into through cracks.
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series Fracture and Structural Integrity
spelling doaj-art-7dcda1d290234ed7a9bc504fa4b041112025-01-02T23:01:30ZengGruppo Italiano FratturaFracture and Structural Integrity1971-89932017-09-01114210.3221/IGF-ESIS.42.03Fatigue crack growth in 2017A-T4 alloy subjected to proportional bending with torsionD. Rozumek0S. Faszynka1Opole University of TechnologyOpole University of TechnologyThe paper presents the results of tests on the fatigue crack growth for a constant moment amplitude under combined bending with torsion in the aluminium alloy AW-2017A-T4. The tests were performed under different values of the load ratio R. Plane specimens with stress concentrators in form of the external one-sided sharp notch were tested. A non-uniform fatigue cracks growth on both lateral surfaces of specimens was observed during experimental tests. Fatigue cracks were developing in the specimens in two stages; quarter-elliptic edge cracks were observed at the beginning, then evolving into through cracks.https://www.fracturae.com/index.php/fis/article/view/1923Fatigue crack growthLoad ratioNotchBending with torsion
spellingShingle D. Rozumek
S. Faszynka
Fatigue crack growth in 2017A-T4 alloy subjected to proportional bending with torsion
Fracture and Structural Integrity
Fatigue crack growth
Load ratio
Notch
Bending with torsion
title Fatigue crack growth in 2017A-T4 alloy subjected to proportional bending with torsion
title_full Fatigue crack growth in 2017A-T4 alloy subjected to proportional bending with torsion
title_fullStr Fatigue crack growth in 2017A-T4 alloy subjected to proportional bending with torsion
title_full_unstemmed Fatigue crack growth in 2017A-T4 alloy subjected to proportional bending with torsion
title_short Fatigue crack growth in 2017A-T4 alloy subjected to proportional bending with torsion
title_sort fatigue crack growth in 2017a t4 alloy subjected to proportional bending with torsion
topic Fatigue crack growth
Load ratio
Notch
Bending with torsion
url https://www.fracturae.com/index.php/fis/article/view/1923
work_keys_str_mv AT drozumek fatiguecrackgrowthin2017at4alloysubjectedtoproportionalbendingwithtorsion
AT sfaszynka fatiguecrackgrowthin2017at4alloysubjectedtoproportionalbendingwithtorsion