Life Assessment of Dynamically Loaded Materials and StructuresL. O. Faria |
Contents
EFFECT OF MANUFACTURING PROCESSES | 537 |
FRACTURE TOUGHNESS AND FATIGUE | 543 |
CRACK INITIATION | 591 |
Copyright | |
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acoustic emission aircraft alloy analysis anisotropy applied assessment behaviour calculated component composite corrosion crack depth crack extension crack front crack growth rate crack initiation crack length crack opening crack propagation crack tip crack velocity creep CTOD cyclic da/dN damage accumulation defect deformation determined distribution effect energy equation experimental eyebar failure fatigue crack growth fatigue crack propagation fatigue life prediction fatigue limit fatigue tests Figure Fracture Mechanics fracture surface fracture toughness geometry impact Kmax KMeq ligament load Magnox material maximum measured method microstructure Miner's rule mode number of cycles observed obtained parameter plane plane strain plastic zone pop-ins present pressure procedure ratio residual stresses room temperature rupture S-N curves sample scanning electron microscope screw sequence shown steel strain strength stress amplitudes stress concentration stress intensity factor structure Table technique tensile tensile stress thermal thickness tubes values variable weld metal