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100 percent coverage Aeronautics and Space Alloy Compressor Blades ALMEN INTENSITY alternating stress level annealed Ti-6A1-4V alloy applied bending bending fatigue specimens blades are recommended change from untreated compressive layer compressive stress layer conducted to determine cracks cross section cycles to failure demarcation line effect on bending extend fatigue extend the fatigue fatigue specimens tested Figure glass bead shot Lewis Research Center lower intensity level material Number multistage compressor NASA Lewis Research Number of cycles parameters of step peen area Peening for Ti-6A1-4V peening intensity peening Ti-6A1-4V compressor Performing Organization Procedures for shot program was conducted residual stress Resulting from Shot root fillet Security Classif shot peening Ti-6A1-4V shot-peened area shot-peened surface SHOT-PEENING METHODS shot-peening parameters Shot-Peening Process Space Administration stainless steel shot surface finish surface to shot-peened tensile stress test program test specimen thickness Ti-6A1-4V Alloy Compressor Ti-6A1-4V compressor blades Titanium two-step process typical airfoil unpeened surface