1993
DOI: 10.1007/bf00012445
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Experimental and finite element study on stable crack growth in three point bending

Abstract: Experimental and finite element results are presented on mode I and mixed mode (involving I and II only) stable crack growth under static loading through an aircraft grade aluminium alloy (D16AT) in three point bending. The results include load-displacement diagrams, J-integrals, plastic zones, tunneling (or crack front curving), etc. During experiment a substantial amount of tunneling is observed, the extent of which increases as the extension progresses in both mode I and mixed mode. The tunneling reduces as… Show more

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Cited by 10 publications
(3 citation statements)
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“…The theoretical investigations have been done with a view to predicting the load-displacement diagrams, plastic zones and the crack edge profiles using a finite element scheme [44][45][46][47] The algorithm works with a variable load increment per step, which is sufficient to bring one or two Gauss points to the yield surface. Further, at the end of each step, any Gauss point whose equivalent stress is greater than 0.995 ~ry is treated as yielded subsequently.…”
Section: Theoretical Investigationsmentioning
confidence: 99%
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“…The theoretical investigations have been done with a view to predicting the load-displacement diagrams, plastic zones and the crack edge profiles using a finite element scheme [44][45][46][47] The algorithm works with a variable load increment per step, which is sufficient to bring one or two Gauss points to the yield surface. Further, at the end of each step, any Gauss point whose equivalent stress is greater than 0.995 ~ry is treated as yielded subsequently.…”
Section: Theoretical Investigationsmentioning
confidence: 99%
“…Each discretisation is made taking note of the initial direction of crack growth so as to permit a study of the whole span of the stable growth through a single discretisation. The direction of initial crack growth can be predicted [10,[44][45][46][47] or obtained experimentally. The elements ahead of the crack tip are squares of size d and those behind it are rhombuses of the same size.…”
Section: Theoretical Investigationsmentioning
confidence: 99%
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