Multiaxial fatigue: An overview and some approximation models for life estimation
By A. Fatemi, Nima Shamsaei. 2011
431 citations recorded by the source corpus.
Subfields: Mechanical Engineering, Mechanics of Materials, Statistics and Probability
View Paper: https://www.semanticscholar.org/paper/677385adcd649ba96e6f68a415101c1578365161
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Mechanical Engineering
- A. Fatemi
- N. Sanaei
- Nima Shamsaei
- N. Phan
- R. Molaei
- Aref Yadollahi
- Jonathan W. Pegues
- Shahriar Sharifimehr
In Mechanics of Materials
- Nima Shamsaei
- N. Phan
- R. Molaei
- A. Fatemi
- Shahriar Sharifimehr
- M. Mehtedi
- Marcello Cabibbo
- E. Santecchia
In Statistics and Probability
- N. Phan
- R. Molaei
- A. Fatemi
- Nima Shamsaei
- Marcello Cabibbo
- E. Santecchia
- Farayi Musharavati
- Erfan Zalnezhad
Citations in the corpus
- Additive manufacturing of fatigue resistant materials: Challenges and opportunities (2017, background): “Variation of FS damage parameter with plane orientation under in-phase (IP) and 90 out-of-phase (OP) axial–torsion loadings at the same strain levels [80].”
- Fatigue of additive manufactured Ti-6Al-4V, Part II: The relationship between microstructure, material cyclic properties, and component performance (2020, background): “Even in parts under uniaxial loading conditions, the stress state may be biaxial or multiaxial due to complex geometries, residual stresses, and stress concentrations [23].”
- A Review on Fatigue Life Prediction Methods for Metals (2016, methodology): “For the multiaxial fatigue life prediction, critical plane approaches linked to the fatigue damage of the material can be found in literature; these approaches are based either on the maximum shear failure plane or on the maximum principal stress (or strain) failure plane [190].”
- Multiaxial fatigue behavior of wrought and additive manufactured Ti-6Al-4V including surface finish effect (2017, methodology): “Thus, among other reasons [24], more slip planes are active during non-proportional loading, as compared to under proportional loading, where only two planes experience maximum shear stress and strain [25].”