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 241
surface crack in the model specimen , as well as the CT specimen . It can be seen that the similar da / dN VS AK relation was observed between the model and the CT specimens . The following Paris ' equation is obtained from Fig.10 ...
surface crack in the model specimen , as well as the CT specimen . It can be seen that the similar da / dN VS AK relation was observed between the model and the CT specimens . The following Paris ' equation is obtained from Fig.10 ...
Page 262
The surface crack ( SC ) specimens were fabricated using the configurations shown in Figure 2. The Ti - 15-3 specimens contained fatigue precracked surface defects whereas the Sic specimens contained surface defects put in by EDM .
The surface crack ( SC ) specimens were fabricated using the configurations shown in Figure 2. The Ti - 15-3 specimens contained fatigue precracked surface defects whereas the Sic specimens contained surface defects put in by EDM .
Page 356
As to the stress intensity factor at the free surface the M. ( 0 ) -value is used . This is the value when alt = 0 which corresponds to the maximum of the line for the relevant weld angle . In principle this value should be equal to the ...
As to the stress intensity factor at the free surface the M. ( 0 ) -value is used . This is the value when alt = 0 which corresponds to the maximum of the line for the relevant weld angle . In principle this value should be equal to the ...
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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