Proceedings of the ... International Conference on Offshore Mechanics and Arctic Engineering, Volume 3American Society of Mechanical Engineers, 2002 - Arctic regions |
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Page 175
... initial machined flaw was observed on the left . A ductile crack grew from the left to the right . In Figs . 5 ( a ) and ( b ) , to and t1 represent the ... Initial flaw Ductile crack 10 mm Initial flaw Ductile. 175 Copyright 2002 by ASME.
... initial machined flaw was observed on the left . A ductile crack grew from the left to the right . In Figs . 5 ( a ) and ( b ) , to and t1 represent the ... Initial flaw Ductile crack 10 mm Initial flaw Ductile. 175 Copyright 2002 by ASME.
Page 481
... initial size of defects which , assuming the crack growth models of Equations ( 3 ) and ( 4 ) , would give predicted fatigue lives in agreement with the experimental lives . The Paris - Erdogan model ( Figure 11 ) is seen to require ...
... initial size of defects which , assuming the crack growth models of Equations ( 3 ) and ( 4 ) , would give predicted fatigue lives in agreement with the experimental lives . The Paris - Erdogan model ( Figure 11 ) is seen to require ...
Page 615
... initial defect size and subsequently fitted a lognormal distribution to the data . This equivalent initial defect size approach has the benefit of relating to the final damage status and using the existing information in experiments ...
... initial defect size and subsequently fitted a lognormal distribution to the data . This equivalent initial defect size approach has the benefit of relating to the final damage status and using the existing information in experiments ...
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alloys analysis applied approximately assessment bending calculated carried coating compared composite compressive considered corrosion crack crack growth curve cycles damage defect deformation depth determined developed direction distribution effect element Engineering equation estimated evaluation experience factor failure fatigue field Figure flaw flexible fracture function geometry given Grade heat higher hydrogen important increase initial installation insulation integrity International joint length limit load locations lower material maximum mean measured mechanical method observed obtained Offshore operation parameters performed pipe plate predicted present pressure problem procedure production properties range reliability residual resistance respectively riser rope safety samples shown shows side simulation solution specimens standard steel strain strength stress structure surface Table temperature tensile tension thermal thickness titanium toughness uncertainties variables weld