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 230
The test specimen was clamped into the load yoke and the test frame so that the girth weld " start and stop " position was always at the " 6 o'clock " ( bottom ) position . By biasing the nominal bending loads ( Ro = 0 ) , fatigue crack ...
The test specimen was clamped into the load yoke and the test frame so that the girth weld " start and stop " position was always at the " 6 o'clock " ( bottom ) position . By biasing the nominal bending loads ( Ro = 0 ) , fatigue crack ...
Page 323
The distribution of SCF's on the chord around the intersection of the stiffened joint , obtained from the two FE models , showed that the SCF's did not drop at the stiffener position as much as measured experimentally ( Fig 12 and 13 ) ...
The distribution of SCF's on the chord around the intersection of the stiffened joint , obtained from the two FE models , showed that the SCF's did not drop at the stiffener position as much as measured experimentally ( Fig 12 and 13 ) ...
Page 381
spot could occur at either the crown or saddle position of the joint , depending upon joint geometry and load type . However , the stresses at both hot spot locations were dominated by the bending component .
spot could occur at either the crown or saddle position of the joint , depending upon joint geometry and load type . However , the stresses at both hot spot locations were dominated by the bending component .
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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