Proceedings of the ... International Conference on Offshore Mechanics and Arctic Engineering, Volume 13, Parts 3-5American Society of Mechanical Engineers, 1994 - Arctic regions |
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Page 82
In all specimens fatigue crack initiated at 10 to 20 percent of the cycles for complete fracture . ( 2 ) The drawback of the SLM is the limited depth of field available during real - time viewing . Specimens with an uneven surface are ...
In all specimens fatigue crack initiated at 10 to 20 percent of the cycles for complete fracture . ( 2 ) The drawback of the SLM is the limited depth of field available during real - time viewing . Specimens with an uneven surface are ...
Page 161
8 : Drop of maximum load in dependence of crack size and number of cycles for a testing machine without internal control 3 . CRACK PROPAGATION IN HOLLOW SECTION JOINTS UNDER CONSTANT AND VARIABLE LOADING A great number of tests have ...
8 : Drop of maximum load in dependence of crack size and number of cycles for a testing machine without internal control 3 . CRACK PROPAGATION IN HOLLOW SECTION JOINTS UNDER CONSTANT AND VARIABLE LOADING A great number of tests have ...
Page 197
One obvious reason for this is the observation of decreasing crack closure stress for small cycles following large cycles ( 19 ] , which in effect will cause a reduction of the threshold level for crack growth .
One obvious reason for this is the observation of decreasing crack closure stress for small cycles following large cycles ( 19 ] , which in effect will cause a reduction of the threshold level for crack growth .
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Contents
FATIGUE AND DEFORMATION | 1 |
Determination of Recovery Length in Spiral Strands | 9 |
FRACTURE ASSESSMENT AND ANALYSIS | 37 |
Copyright | |
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Common terms and phrases
analysis applied assessment bending calculated compared composition considered constant corrosion crack growth CTOD curve cycles deformation dependence deposit depth determined developed distribution effect elastic electrode Engineering environment equation experimental factor failure fatigue crack Figure finite element fracture geometry given grain heat higher hydrogen increase indicate initial International joints length limit load lower material mean measured Mechanics method microstructure nitrogen notch observed obtained occur Offshore operating oxygen parameters performed phase pipe plastic plate predictions present pressure problems procedure produced propagation properties protection range ratio reduced region Research residual respectively sea water shown shows simulated specimens standard steel strain strength stress structures surface Table temperature tensile thickness toughness tubular joints values weld metal wire yield