Proceedings of the ... International Conference on Offshore Mechanics and Arctic Engineering, Volumes 3-4American Society of Mechanical Engineers, 1992 - Arctic regions |
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Page 55
Second , the area fraction of fully recovered regions in the crack plane increases with slowering thermal cycle . ... Cycles 3 and 4 with Steel D ( Figure 3d ) had slightly different correlations than the rest and perhaps exceptions to ...
Second , the area fraction of fully recovered regions in the crack plane increases with slowering thermal cycle . ... Cycles 3 and 4 with Steel D ( Figure 3d ) had slightly different correlations than the rest and perhaps exceptions to ...
Page 252
The hot spot stress range was 240 MPa and the stress ratio , R , which is the ratio of minimum to maximum load in the fatigue cycle , was -1 . Loading was discontinued after 184,000 cycles at which point the maximum saddle crack depth ...
The hot spot stress range was 240 MPa and the stress ratio , R , which is the ratio of minimum to maximum load in the fatigue cycle , was -1 . Loading was discontinued after 184,000 cycles at which point the maximum saddle crack depth ...
Page 290
8 The Treatment of Variable Amplitude Loading The number of cycles of each block of stress and the total number of cycles do not provide a limit for the end of the fatigue calculation , instead they provide the " weighting " in the ...
8 The Treatment of Variable Amplitude Loading The number of cycles of each block of stress and the total number of cycles do not provide a limit for the end of the fatigue calculation , instead they provide the " weighting " in the ...
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Contents
WELD METAL AND HAZ PROPERTIES | 1 |
ADVANCES IN STEEL AND WELDING | 65 |
Kapadia Y Adonyi J D Defilippi and W F Domis | 73 |
Copyright | |
36 other sections not shown
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addition alloys analysis applied assessment axial base base metal behaviour bending calculated carried compared composite considered corrosion crack growth CTOD curve cycles defect depth determined distribution effect element energy Engineering equations estimate experimental factor failure fatigue crack Figure fracture function geometry grain hardness heat higher increase indicated initiation input interaction joint length limit load material mean measured mechanical method microstructure notch observed obtained occur offshore parameters performed pipe plastic plate predictions present pressure probability procedure produced properties range ratio region reported Research seal seawater shown shows significant solution specimens steel strain stress stress intensity structures surface Table temperature tensile thickness thread toughness tubular joints values weld metal wire yield strength zone