NASA NTRS · 19840005539
Three-dimensional analysis of chevron-notched specimens by boundary integral method
Abstract
The chevron-notched short bar and short rod specimens was analyzed by the boundary integral equations method. This method makes use of boundary surface elements in obtaining the solution. The boundary integral models were composed of linear triangular and rectangular surface segments. Results were obtained for two specimens with width to thickness ratios of 1.45 and 2.00 and for different crack length to width ratios ranging from 0.4 to 0.7. Crack opening displacement and stress intensity factors determined from displacement calculations along the crack front and compliance calculations were compared with experimental values and with finite element analysis.
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Mendelson, A., Ghosn, L.. 1983-09-01. Three-dimensional analysis of chevron-notched specimens by boundary integral method. https://ntrs.nasa.gov/citations/19840005539
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