A comprehensive fracture-mechanics-based life prediction methodology is presented for fcc single crystal components based on the computation of stress intensity factors (SIFs), and the modeling of the crystallographic fatigue crack growth (FCG) process under mixed-mode loading conditions. The 3D finite element numerical procedure presented for computing SIFs for anisotropic materials under mixed-mode loading is very general and not just specific to fcc single crystals. SIFs for a Brazilian disk specimen are presented for the crack on the {111}) plane in the ⟨101⟩ and ⟨121⟩ directions, which represent the primary and secondary slip directions. Variation of SIFs as a function of thickness is also presented. Modeling of the crystallographic FCG behavior is performed by using the resolved shear stress intensity coefficient, . This parameter is sensitive to the grain orientation and is based on the resolved shear stresses on the slip planes at the crack tip, which is useful in identifying the active crack plane as well as in predicting the crack growth direction. A multiaxial fatigue crack driving force parameter, , was quantified, which can be used to predict the FCG rate and, hence, life in single crystal components subject to mixed-mode fatigue loading.
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e-mail: srikant@ufl.edu
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A Fracture-Mechanics-Based Methodology for Fatigue Life Prediction of Single Crystal Nickel-Based Superalloys
Srikant Ranjan,
Srikant Ranjan
Mechanical and Aerospace Engineering Department,
e-mail: srikant@ufl.edu
University of Florida
, Gainesville, FL 32611-6300
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Nagaraj K. Arakere
Nagaraj K. Arakere
Mechanical and Aerospace Engineering Department,
e-mail: nagaraj@ufl.edu
University of Florida
, Gainesville, FL 32611-6300
Search for other works by this author on:
Srikant Ranjan
Mechanical and Aerospace Engineering Department,
University of Florida
, Gainesville, FL 32611-6300e-mail: srikant@ufl.edu
Nagaraj K. Arakere
Mechanical and Aerospace Engineering Department,
University of Florida
, Gainesville, FL 32611-6300e-mail: nagaraj@ufl.edu
J. Eng. Gas Turbines Power. May 2008, 130(3): 032501 (11 pages)
Published Online: March 26, 2008
Article history
Received:
October 16, 2006
Revised:
October 17, 2006
Published:
March 26, 2008
Citation
Ranjan, S., and Arakere, N. K. (March 26, 2008). "A Fracture-Mechanics-Based Methodology for Fatigue Life Prediction of Single Crystal Nickel-Based Superalloys." ASME. J. Eng. Gas Turbines Power. May 2008; 130(3): 032501. https://doi.org/10.1115/1.2838990
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