1.1 with additional edge refinements at the edges surrounding the defect at 0.75. Simulations were run using non-reduced integration methods. Fig. 39.2 (a) Profile view of the machined defect dimensions, (b) axial profile of the machined defect dimensions Fig. 39.3 Schematic of the multi-vessel fatigue system Fig. 39.4 Schematic of strain gage locations 39 Performance of Patch and Full-Encirclement Bonded Composite Repairs 339
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