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 22
... given up to L , = 1 through the corresponding level 0 equations , ( 14 ) and ( 15 ) , respectively . An equation is proposed for the failure line in the range L , 1 given by : N - 1 K1 = K ( LL2N ` r ( L , -1 ) ' 1.1 1.2 1.3 1.4 1.5 L T ...
... given up to L , = 1 through the corresponding level 0 equations , ( 14 ) and ( 15 ) , respectively . An equation is proposed for the failure line in the range L , 1 given by : N - 1 K1 = K ( LL2N ` r ( L , -1 ) ' 1.1 1.2 1.3 1.4 1.5 L T ...
Page 27
... given temperature , specimen thickness and probability level can be obtained from : 0.25 Kmat = 20 ( 11 + 77 exp [ 0.019 ( T – T , ) ) 25 B ( 23 ) 23 ( -in ( 1 – P , ) , ' 0.25 [ 10 ] However , in the examples given in the next section ...
... given temperature , specimen thickness and probability level can be obtained from : 0.25 Kmat = 20 ( 11 + 77 exp [ 0.019 ( T – T , ) ) 25 B ( 23 ) 23 ( -in ( 1 – P , ) , ' 0.25 [ 10 ] However , in the examples given in the next section ...
Page 177
... given design case during a specified service life can be obtained by multiplying the probability of the composite joint failing during the expected duration of the loading by the probability of occurrence of a given load within the ...
... given design case during a specified service life can be obtained by multiplying the probability of the composite joint failing during the expected duration of the loading by the probability of occurrence of a given load within the ...
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