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 308
... locations Figure 1 - C2 specimen Detailed information of the modelling and discussion of the results can be seen in [ 12 ] and an improvement of the studied structures with respect to fatigue damage can be found in [ 13 ] . Hot spot ...
... locations Figure 1 - C2 specimen Detailed information of the modelling and discussion of the results can be seen in [ 12 ] and an improvement of the studied structures with respect to fatigue damage can be found in [ 13 ] . Hot spot ...
Page 309
... Locations of the high stress areas on C2 models Figure 5 shows the locations of the high stressed areas ( HSA ) on the C2.1 and the C2.2 models . Three out of four of them are located on the upper plate . Two of them are located above ...
... Locations of the high stress areas on C2 models Figure 5 shows the locations of the high stressed areas ( HSA ) on the C2.1 and the C2.2 models . Three out of four of them are located on the upper plate . Two of them are located above ...
Page 310
... locations A , D , E and H are at the horizontal and the vertical plate of the specimen , while the cracks B , C , G and F are located on the diagonal plate of the specimen . Even if the four crack locations ( within each of these two ...
... locations A , D , E and H are at the horizontal and the vertical plate of the specimen , while the cracks B , C , G and F are located on the diagonal plate of the specimen . Even if the four crack locations ( within each of these two ...
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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