Life Assessment of Dynamically Loaded Materials and StructuresL. O. Faria |
Contents
Properties and fracture of automotive connecting rods | 535 |
FRACTURE TOUGHNESS AND FATIGUE | 543 |
STRESS INTENSITY FACTORS | 548 |
Copyright | |
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actual aircraft alloy amplitude analysis applied assessment behaviour calculated compared component composite considered constant corresponding crack growth crack initiation crack length crack propagation crack tip creep curves cycles damage defect dependent depth described determined developed direction displacement distribution effect energy equation estimated example experimental experiments extension factor failure fatigue crack fatigue crack growth Figure final fracture Fracture Mechanics function geometry given gives growth rates increase initiation inspection limit load material maximum mean measured Mechanics method mode observed obtained occur operation parameter performed plastic plate prediction present pressure probability problem procedure properties range ratio recorded REFERENCES reported shown shows specimen spectrum steel strain strength stress intensity factor structure surface Table taken technique temperature tensile thickness toughness tubes values weld yield zone