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Approximate stress-intensity factor solutions for nozzle corner cracks
In this paper first the iso-stress lines at a nozzle corner are simplified into slanted straight lines at an angle of 45° with the walls of cylinder and nozzle and the natural nozzle corner cracks as quarter-circular ones. On the basis of this, a stress-intensity factor solution for an arbitrary poi...
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Published in: | The International journal of pressure vessels and piping 1990, Vol.42 (1), p.75-96 |
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Main Authors: | , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | In this paper first the iso-stress lines at a nozzle corner are simplified into slanted straight lines at an angle of 45° with the walls of cylinder and nozzle and the natural nozzle corner cracks as quarter-circular ones. On the basis of this, a stress-intensity factor solution for an arbitrary point on the crack front is derived by means of approximate analysis. Following from this, approximate expressions of the maximum and average stress-intensity factors
K
i
max
and
K
im
are proposed, which are very important to the analysis of fatigue and fracture of practical pressure vessel nozzle corner cracks. These expressions show good consistency with the results of FEM, Kobayashi's approximate analysis and Besuner's IFM for about 40 cracks from nine nozzle sections. The expressions of
K
i
max
and
K
im
are not only very simple but also have excellent accuracy; for most cracks the error is less than 10%. |
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ISSN: | 0308-0161 1879-3541 |
DOI: | 10.1016/0308-0161(90)90056-N |