Proceedings of the ... International Conference on Offshore Mechanics and Arctic Engineering, Volume 18, Part 3American Society of Mechanical Engineers, 2000 - Arctic regions |
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Page 159
... loading = 0.808 + 1.0530 -1.02902 ) ( 0.8 b . in - plane bending R = ( 6.22-10.600 +5.03492 ) R45 ยท ( 5 ) ( 6 ) c . out - of - plane bending R = ( 1.516 + 0.6630 ) ( 7 ) R45 e in Eqns . ( 5 ) - ( 7 ) are in radians . ( Validity range ...
... loading = 0.808 + 1.0530 -1.02902 ) ( 0.8 b . in - plane bending R = ( 6.22-10.600 +5.03492 ) R45 ยท ( 5 ) ( 6 ) c . out - of - plane bending R = ( 1.516 + 0.6630 ) ( 7 ) R45 e in Eqns . ( 5 ) - ( 7 ) are in radians . ( Validity range ...
Page 162
... loading , which indicated that joints with a large B - ratio would fail from the brace side and with an anomalously low fatigue strength . In the present study fatigue behaviour of CRHS joints subjected to axial and in - plane bending ...
... loading , which indicated that joints with a large B - ratio would fail from the brace side and with an anomalously low fatigue strength . In the present study fatigue behaviour of CRHS joints subjected to axial and in - plane bending ...
Page 192
... loading mode . Similar to the static multiaxial failure envelope obtained in [ 10 ] under monotonic loading , the cyclic multiaxial fatigue failure envelopes are highly distorted , indicating a significant amount of interaction among ...
... loading mode . Similar to the static multiaxial failure envelope obtained in [ 10 ] under monotonic loading , the cyclic multiaxial fatigue failure envelopes are highly distorted , indicating a significant amount of interaction among ...
Contents
STRUCTURAL INTEGRITY PROCEDURES FOR EUROPE SINTAP | 1 |
OMAE99MAT2041 | 9 |
Development of the SINTAP Failure Assessment Diagrams for Compatibility With | 19 |
Copyright | |
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addition analysis applications approach ASME assessment base behavior bending CGHAZ Charpy compared component composite condition Conference Copyright crack critical CTOD curve defects deposition depth determined developed distribution dynamic effect element energy Engineering equations equivalent evaluated factors failure fatigue ferrite Figure fire fracture toughness function geometry given hardness heat input impact important improve increase initiation International joints length limit loading lower material matrix maximum mean measured mechanical method microstructure molten observed obtained offshore operating parameters performance phase pipe plate prediction present pressure procedure production properties protection range ratio reduced region requirements residual stress respectively risers safety ship shown shows specimens standards steel strain strength structures surface Table temperature tensile thickness values weld metal welded joints wire yield