Based on a recently developed shakedown theory for non-smooth nonlinear materials, we derive a criterion for high-cycle fatigue in shape memory alloys (SMAs). The fatigue criterion takes into account phase transformation as well as reorientation of martensite variants as the source of fatigue damage. The mathematical derivation of the criterion is based on the requirement of elastic shakedown for a given structure to achieve unlimited fatigue endurance. Elastic shakedown is defined as an asymptotic state in which damage due to time-varying load becomes confined at the mesoscopic scale, or the scale of the grain, with no discernable inelasticity at the macroscopic scale. From an energy standpoint, elastic shakedown corresponds to a situation where energy dissipation becomes bounded and the response elastic after a certain number of loading cycles. A sufficient condition to achieve this state was established by Melan (1936) [1] and Koiter (1960) [2] for elastoplastic materials and later generalized to hardening plasticity by Nguyen (2003) and to non-smooth non-linear materials by Peigney (2014). The latter formulation is applicable to SMAs obeying the ZM constitutive model (Zaki & Moumni, 2007) and is shown here to allow the derivation of a high-cycle fatigue criterion analogous to the one proposed by Dang Van (1973) for elastoplastic materials. The criterion allows establishing a safe domain in stress deviator space at the mesoscopic scale consisting of a hypercylinder with axis parallel to the direction of martensite orientation. The hypercylinder is delimited along its axis by two transverse hyperplanes representing bounds on admissible stress states consistent with the loading conditions for phase transformation. Safety with regard to high-cycle fatigue, upon elastic shakedown, is conditioned by the persistence of the macroscopic stress path, as the load varies and at every material point, strictly within the hypercylinder. The size of the hypercylinder is shown to strongly depend on the relative amount of martensite present in the SMA.
Skip Nav Destination
ASME 2016 Conference on Smart Materials, Adaptive Structures and Intelligent Systems
September 28–30, 2016
Stowe, Vermont, USA
Conference Sponsors:
- Aerospace Division
ISBN:
978-0-7918-5049-7
PROCEEDINGS PAPER
High-Cycle Fatigue Criterion for Shape Memory Alloys Based on Shakedown Theory
Wael Zaki,
Wael Zaki
Khalifa University (KUSTAR), Abu Dhabi, UAE
Search for other works by this author on:
Xiaojun Gu,
Xiaojun Gu
Northwestern Polytechnical University, Xi’an, Shaanxi, China
ENSTA-ParisTech, Palaiseau Cedex, France
Search for other works by this author on:
Ziad Moumni,
Ziad Moumni
ENSTA-ParisTech, Palaiseau Cedex, France
Search for other works by this author on:
Weihong Zhang
Weihong Zhang
Northwestern Polytechnical University, Xi’an, Shaanxi, China
Search for other works by this author on:
Wael Zaki
Khalifa University (KUSTAR), Abu Dhabi, UAE
Xiaojun Gu
Northwestern Polytechnical University, Xi’an, Shaanxi, China
ENSTA-ParisTech, Palaiseau Cedex, France
Ziad Moumni
ENSTA-ParisTech, Palaiseau Cedex, France
Weihong Zhang
Northwestern Polytechnical University, Xi’an, Shaanxi, China
Paper No:
SMASIS2016-9165, V002T03A015; 6 pages
Published Online:
November 29, 2016
Citation
Zaki, W, Gu, X, Moumni, Z, & Zhang, W. "High-Cycle Fatigue Criterion for Shape Memory Alloys Based on Shakedown Theory." Proceedings of the ASME 2016 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. Volume 2: Modeling, Simulation and Control; Bio-Inspired Smart Materials and Systems; Energy Harvesting. Stowe, Vermont, USA. September 28–30, 2016. V002T03A015. ASME. https://doi.org/10.1115/SMASIS2016-9165
Download citation file:
15
Views
Related Proceedings Papers
Related Articles
Determinist-Probabilistic Concept in Modeling Fatigue Damage Through a Micromechanical Approach
J. Eng. Mater. Technol (January,2010)
Finite Element Modeling of Fatigue Damage Using a Continuum Damage Mechanics Approach
J. Pressure Vessel Technol (May,2005)
Related Chapters
Artificial Indents as the Root Cause of Rolling Contact Fatigue Damage: Effect of Plastic Properties
Bearing and Transmission Steels Technology
Fatigue Damage Mechanisms in Composite Materials: A Review
Fatigue Mechanisms
Estimation of K Ic from Slow Bend Precracked Charpy Specimen Strength Ratios
Developments in Fracture Mechanics Test Methods Standardization