A critical plane-based high-cycle multiaxial fatigue criterion, known as the Carpinteri–Spagnoli (C–S)criterion, is here extended to evaluate the fatigue lifetime of plain metallic components under constantamplitude loading in the low/medium-cycle regime. This extended criterion, based on strain components,resolves the strain tensor into the normal and shear components acting on the critical plane, which isdetermined on the basis of the principal strain courses over the loading cycle. An equivalent normal strainamplitude, computed through a quadratic combinations of strain components in the critical plane, istaken as the fatigue damage parameter. The required input parameters of the criterion are obtained fromthe classical Manson–Coffin–Basquin law for axial loading. A validation by experimental data pertainingthe biaxial fatigue of plain steel specimens under both proportional and non-proportional loadings isperformed.

Lifetime Estimation in the Low/Medium-Cycle Regime Using the Carpinteri-Spagnoli Multiaxial Fatigue Criterion

RONCHEI, Camilla;
2014-01-01

Abstract

A critical plane-based high-cycle multiaxial fatigue criterion, known as the Carpinteri–Spagnoli (C–S)criterion, is here extended to evaluate the fatigue lifetime of plain metallic components under constantamplitude loading in the low/medium-cycle regime. This extended criterion, based on strain components,resolves the strain tensor into the normal and shear components acting on the critical plane, which isdetermined on the basis of the principal strain courses over the loading cycle. An equivalent normal strainamplitude, computed through a quadratic combinations of strain components in the critical plane, istaken as the fatigue damage parameter. The required input parameters of the criterion are obtained fromthe classical Manson–Coffin–Basquin law for axial loading. A validation by experimental data pertainingthe biaxial fatigue of plain steel specimens under both proportional and non-proportional loadings isperformed.
2014
Multiaxial low-cycle fatigue; Critical plane approach; Strain-based criterion; Constant amplitude loading
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.11770/304661
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