A critical distance/plane method to estimate finite life of notched components under variable amplitude uniaxial/multiaxial fatigue loading

Author:

Susmel Luca,Taylor David

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modelling and Simulation

Reference65 articles.

1. Estimated and experimental fatigue lives of 30CrNiMo8 steel under in- and out-of-phase combined bending and torsion with variable amplitude;Łagoda;Fatigue Fract Eng Mater Struct,1994

2. A critical plane approach for life prediction of high cycle fatigue under multiaxial variable amplitude loading;Morel;Int J Fatigue,2000

3. A multiaxial fatigue criterion for random loading;Carpinteri;Fatigue Fract Engng Mater Struct,2003

4. Criteria of multiaxial random fatigue based on stress, strain and energy parameters of damage in the critical plane;Łagoda;Mat-wiss u Werkstofftech,2005

5. Fatigue lives of 18G2A and 10HNAP steels under variable amplitude and random non-proportional bending with torsion;Marciniak;Int J Fatigue,2008

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