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EFFECT OF MANUFACTURING PROCESSES
FRACTURE TOUGHNESS AND FATIGUE
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acoustic emission aircraft alloy analysis anisotropy applied assessment behaviour calculated component composite corresponding corrosion crack depth crack extension crack front crack growth rate crack initiation crack length crack opening crack propagation crack tip crack velocity creep cyclic da/dN damage accumulation defect deformation determined distribution effect energy equation estimated experimental eyebar failure fatigue crack growth fatigue crack propagation fatigue life prediction fatigue limit fatigue tests Figure fracture mechanics fracture surface fracture toughness geometry grain impact inclusions KMeq ligament Magnox maximum measured method microstructure Miner's rule mode modulus number of cycles observed obtained operation parameter plane plane strain plastic zone present pressure procedure properties ratio residual stresses room temperature rupture S-N curves scanning electron microscope screw shown shows spectrum steel strain strength stress amplitudes stress concentration stress intensity factor structure Table technique tensile tensile stress thickness tubes values variable weld yield stress