This paper investigates the effect of strain gage length on residual stress estimated by the slitting (or crack compliance) method. This effect is quantified for a range of gage length normalized by sample thickness, , between 0.005 and 0.100. For specific values, compliance matrix elements are determined by finite element methods for a range of crack depth and polynomial basis functions for residual stress. Resulting compliance matrices are shown and used to determine error in residual stress that may arise due to differences in assumed in data reduction and existing in the slitting experiment. Errors increase monotonically with increasing difference between assumed and actual and reach a root-mean-square error of 14% of peak stress. In order to avoid such errors, a scheme is presented that allows compliance matrices to be computed for from tabulated coefficients and limits root-mean-square error to of peak stress. An example is provided to illustrate the application of the data reduction scheme to laboratory data.
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e-mail: mrhill@ucdavis.edu
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January 2007
Technical Papers
Effect of Strain Gage Length When Determining Residual Stress by Slitting
Matthew J. Lee,
Matthew J. Lee
Mechanical and Aeronautical Engineering,
University of California
, One Shields Avenue, Davis, CA 95616
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Michael R. Hill
Michael R. Hill
Mechanical and Aeronautical Engineering,
e-mail: mrhill@ucdavis.edu
University of California
, One Shields Avenue, Davis, CA 95616
Search for other works by this author on:
Matthew J. Lee
Mechanical and Aeronautical Engineering,
University of California
, One Shields Avenue, Davis, CA 95616
Michael R. Hill
Mechanical and Aeronautical Engineering,
University of California
, One Shields Avenue, Davis, CA 95616e-mail: mrhill@ucdavis.edu
J. Eng. Mater. Technol. Jan 2007, 129(1): 143-150 (8 pages)
Published Online: July 12, 2006
Article history
Received:
May 12, 2005
Revised:
July 12, 2006
Citation
Lee, M. J., and Hill, M. R. (July 12, 2006). "Effect of Strain Gage Length When Determining Residual Stress by Slitting." ASME. J. Eng. Mater. Technol. January 2007; 129(1): 143–150. https://doi.org/10.1115/1.2400263
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