Proceedings of the ... International Conference on Offshore Mechanics and Arctic Engineering, Volume 9American Society of Mechanical Engineers, 1990 - Arctic regions |
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Page 186
consame will experience a smaller stress than the initial crack of the length in the thicker plate , causing a smaller initial crack growth rate in the former case . The difference in initial crack growth rate overmatches the difference ...
consame will experience a smaller stress than the initial crack of the length in the thicker plate , causing a smaller initial crack growth rate in the former case . The difference in initial crack growth rate overmatches the difference ...
Page 291
Figure 6 : Initial crack depth versus number of years for through the thickness crack growth , ai / c ; = 0.4 and design Miner sum equal to 0.05 and 0.025 . AUC 0.20 AL / C -0.40 AU / C -0.60 ALC : 1.00 10-1 LOW LO 1.0 0.8 CRACK ASPECT ...
Figure 6 : Initial crack depth versus number of years for through the thickness crack growth , ai / c ; = 0.4 and design Miner sum equal to 0.05 and 0.025 . AUC 0.20 AL / C -0.40 AU / C -0.60 ALC : 1.00 10-1 LOW LO 1.0 0.8 CRACK ASPECT ...
Page 382
Therefore , in this analysis , fatigue life of a T - joint is defined as the number of load cycles required to propagate the crack from an assumed initial depth to penetration through the member thickness , i.e. , N3 .
Therefore , in this analysis , fatigue life of a T - joint is defined as the number of load cycles required to propagate the crack from an assumed initial depth to penetration through the member thickness , i.e. , N3 .
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Contents
ADVANCED COMPOSITES | 1 |
The Use of GRP Materials in Platform Topsides Construction and the Regulatory Implications | 15 |
SAFETY AND RELIABILITY | 17 |
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analysis applications axial behaviour bending brace calculated chord combined compared components composite Composite Materials compression concrete connection considered construction corrosion crack critical curve cycles damage determined developed distribution effect element Engineering environment experimental factor failure fatigue fiber Figure finite element force fracture geometry increase indicate influence initial internal laminate length limit load lower Marine material matrix maximum mean measured mechanical method Mode nodes nominal normal observed obtained offshore operation parameters performance pipe plate platform predicted present pressure production properties range ratio reduced reinforcement Research resin resistance seal shear shell shown shows solutions specimens steel stiffener stiffness strain strength stress stress concentration structures surface Table techniques temperature tensile tension thickness thread tube tubular joints weight weld