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Characterization of Residual Stress Effects on Fatigue Crack Growth of a Friction Stir Welded Aluminum AlloyAn on-line compliance-based method to account for residual stress effects in stress-intensity factor and fatigue crack growth property determinations has been evaluated. Residual stress intensity factor results determined from specimens containing friction stir weld induced residual stresses are presented, and the on-line method results were found to be in excellent agreement with residual stress-intensity factor data obtained using the cut compliance method. Variable stress-intensity factor tests were designed to demonstrate that a simple superposition model, summing the applied stress-intensity factor with the residual stress-intensity factor, can be used to determine the total crack-tip stress-intensity factor. Finite element, VCCT (virtual crack closure technique), and J-integral analysis methods have been used to characterize weld-induced residual stress using thermal expansion/contraction in the form of an equivalent delta T (change in local temperature during welding) to simulate the welding process. This equivalent delta T was established and applied to analyze different specimen configurations to predict residual stress distributions and associated residual stress-intensity factor values. The predictions were found to agree well with experimental results obtained using the crack- and cut-compliance methods.
Document ID
20150002817
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Newman, John A.
(NASA Langley Research Center Hampton, VA, United States)
Smith, Stephen W.
(NASA Langley Research Center Hampton, VA, United States)
Seshadri, Banavara R.
(National Inst. of Aerospace Hampton, VA, United States)
James, Mark A.
(Alcoa Technical Center Alcoa Center, PA, United States)
Brazill, Richard L.
(Alcoa Technical Center Alcoa Center, PA, United States)
Schultz, Robert W.
(Alcoa Technical Center Alcoa Center, PA, United States)
Donald, J. Keith
(Fracture Technology Associates Bethlehem, PA, United States)
Blair, Amy
(Fracture Technology Associates Bethlehem, PA, United States)
Date Acquired
March 11, 2015
Publication Date
February 1, 2015
Subject Category
Metals And Metallic Materials
Report/Patent Number
NASA/TM-2015-218685
L-20495
NF1676L-20137
Funding Number(s)
WBS: WBS 432938.11.01.07.43.40.09
Distribution Limits
Public
Copyright
Public Use Permitted.
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