2015
DOI: 10.1016/j.ijfatigue.2015.01.005
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Crack growth behavior under biaxial fatigue with phase difference

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Cited by 31 publications
(19 citation statements)
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“…The 2 cracks then propagate symmetric to the 45° plane with an angle of 90° between them. This splitting of the crack into 2 cracks was also observed by Mall and Perel for in‐plane biaxial fatigue tests with 180° phase difference. The orientation of the cracks in this case can be explained using the maximum hoop stress theory, which states that the crack tends to propagate in the direction that results in maximum hoop stress at the crack tip, leading to minimization of the K II component of the crack driving force.…”
Section: Resultssupporting
confidence: 81%
“…The 2 cracks then propagate symmetric to the 45° plane with an angle of 90° between them. This splitting of the crack into 2 cracks was also observed by Mall and Perel for in‐plane biaxial fatigue tests with 180° phase difference. The orientation of the cracks in this case can be explained using the maximum hoop stress theory, which states that the crack tends to propagate in the direction that results in maximum hoop stress at the crack tip, leading to minimization of the K II component of the crack driving force.…”
Section: Resultssupporting
confidence: 81%
“…Gotoh, Niwa, and Anai () evaluated the effect of phase difference on the biaxial FCG rate of steel under six different loading conditions, and it is found that the FCG rate was the largest under 180° phase difference. Mall and Perel () investigated the FCG behavior of aluminum alloy 7075‐T6 under in‐plane biaxial tension with phase differences of 90° and 180°. It was found that the cracks exhibited bifurcation behavior under both 90° and 180° phase differences, but the FCG rates after splitting were almost the same under both phase differences.…”
Section: Discussionmentioning
confidence: 99%
“…Biaxial FCG path in the presence of phase difference is also one of the hot research fields currently. Mall and Perel () observed the bifurcation behavior of 45° slant crack during in‐plane biaxial tension fatigue with phase differences of 90° and 180°. Infante‐García, Qian, Miguélez, and Giner () simulated the FCG behavior of 45° slant cracks under biaxial loading using a finite element method based on linear elastic fracture mechanics.…”
Section: Discussionmentioning
confidence: 99%
“…The determination of the stress intensity factors for other specimen geometries as well as components K comp is performed by means of the crack length-dependent as well as geometry-dependent correction function Y (a), see Eq. (5). The determination of the Y values for specific crack length a for cruciform specimens can by done by Eq.…”
Section: Scaling Of the Forces Stresses And Stress Intensity Factorsmentioning
confidence: 99%
“…Refs. [3][4][5][6][7], and (iii) specimen design with thickness-reduced measuring area and slotted arms, see e.g. Refs.…”
Section: Introductionmentioning
confidence: 99%