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 45
... cycles ) that is normally used to predict the fatigue life of mooring line components . This methodology is exclusively based on the load applied to the component and does not consider the stress state of the component promoted by the ...
... cycles ) that is normally used to predict the fatigue life of mooring line components . This methodology is exclusively based on the load applied to the component and does not consider the stress state of the component promoted by the ...
Page 154
... cycles to crack initiation obtained by the tests . The critical strain value for the crack initiation under large bending deformation as mentioned in chap.4 is also shown in Fig.27 , and both axes in the figure are shown logarithmically ...
... cycles to crack initiation obtained by the tests . The critical strain value for the crack initiation under large bending deformation as mentioned in chap.4 is also shown in Fig.27 , and both axes in the figure are shown logarithmically ...
Page 530
... cycles , N 20 Specimen 5611 - T1-4 18 Experimental 16 2D - M 143 12 100 8 00 80 70 60 ○ Experimental 50 Crack length , 2c mm 30 50 40 9090 30 2D - M 20 10 / Specimen 5611 - T1-3 Pang 0 5x105 10 € 1.5x10 2x106 Number of cycles , N Fig.2 ...
... cycles , N 20 Specimen 5611 - T1-4 18 Experimental 16 2D - M 143 12 100 8 00 80 70 60 ○ Experimental 50 Crack length , 2c mm 30 50 40 9090 30 2D - M 20 10 / Specimen 5611 - T1-3 Pang 0 5x105 10 € 1.5x10 2x106 Number of cycles , N Fig.2 ...
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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