A finite element analysis of steady-state crack growth in pseudoelastic shape memory alloys under the assumption of adiabatic conditions is carried out for plane strain, mode I loading. The crack is assumed to propagate at a critical level of the crack-tip energy release rate and the fracture toughness is obtained as the ratio of the far-field applied energy release rate to the crack-tip critical value. Results related to the influence of latent heat on the near-tip stress field and fracture toughness are presented for a range of parameters related to thermomechanical coupling. The levels of fracture toughness enhancement, associated with the energy dissipated by the transformed material in the wake of the growing crack, are found to be lower under adiabatic conditions than under isothermal conditions [Baxevanis et al., 2014, J. Appl. Mech., 81, 041005]. Given that in real applications of shape memory alloy (SMA) components the processes are usually not adiabatic, which is the case with the lowest energy dissipation during a cyclic loading–unloading process (hysteresis), it is expected that the actual level of transformation toughening would be higher than the one corresponding to the adiabatic case.
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October 2014
Research-Article
On the Effect of Latent Heat on the Fracture Toughness of Pseudoelastic Shape Memory Alloys
Theocharis Baxevanis,
Theocharis Baxevanis
Department of Aerospace Engineering,
e-mail: theocharis@tamu.edu
Texas A&M University
,College Station, TX 77843-3141
e-mail: theocharis@tamu.edu
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Chad M. Landis,
Chad M. Landis
Department of Aerospace Engineering
and Engineering Mechanics,
e-mail: landis@utexas.edu
and Engineering Mechanics,
The University of Texas at Austin
,Austin, TX 78712-0235
e-mail: landis@utexas.edu
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Dimitris C. Lagoudas
Dimitris C. Lagoudas
Department of Aerospace Engineering,
e-mail: lagoudas@tamu.edu
Texas A&M University
,College Station, TX 77843-3141
e-mail: lagoudas@tamu.edu
Search for other works by this author on:
Theocharis Baxevanis
Department of Aerospace Engineering,
e-mail: theocharis@tamu.edu
Texas A&M University
,College Station, TX 77843-3141
e-mail: theocharis@tamu.edu
Chad M. Landis
Department of Aerospace Engineering
and Engineering Mechanics,
e-mail: landis@utexas.edu
and Engineering Mechanics,
The University of Texas at Austin
,Austin, TX 78712-0235
e-mail: landis@utexas.edu
Dimitris C. Lagoudas
Department of Aerospace Engineering,
e-mail: lagoudas@tamu.edu
Texas A&M University
,College Station, TX 77843-3141
e-mail: lagoudas@tamu.edu
Contributed by the Applied Mechanics Division of ASME for publication in the JOURNAL OF APPLIED MECHANICS. Manuscript received May 27, 2014; final manuscript received July 31, 2014; accepted manuscript posted August 7, 2014; published online August 13, 2014. Editor: Yonggang Huang.
J. Appl. Mech. Oct 2014, 81(10): 101006 (6 pages)
Published Online: August 13, 2014
Article history
Received:
May 27, 2014
Revision Received:
July 31, 2014
Accepted:
August 7, 2014
Citation
Baxevanis, T., Landis, C. M., and Lagoudas, D. C. (August 13, 2014). "On the Effect of Latent Heat on the Fracture Toughness of Pseudoelastic Shape Memory Alloys." ASME. J. Appl. Mech. October 2014; 81(10): 101006. https://doi.org/10.1115/1.4028191
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