The ASME Section III Design-by-Analysis rules for pressure-retaining components include a detailed fatigue evaluation based on elastically predicted primary, secondary, and peak stresses. A prerequisite for the fatigue analysis is that the primary-plus-secondary stress range does not exceed . If this limit is exceeded, the code provides “Simplified Elastic-Plastic Analysis” rules for the fatigue evaluation. A penalty factor is applied to the elastically predicted alternating stress. The maximum value of (3.3 or 5) is a severe design limitation. Test data indicate that the code specified maximum value of is very conservative. The simplified elastic-plastic rules were originally developed for piping and published in B31.7. When the piping rules were incorporated into Section III in 1971, the B31.7 procedure was replaced by a less complex procedure. The development of the simplified elastic-plastic analysis approach is reviewed to establish the technical basis for the present code rules. The concepts of fatigue, shakedown to elastic action, thermal bending, elastic follow-up, notch factor, and strain redistribution are discussed. Recommendations for changes to the plastic strain correction factor are provided.
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February 2006
Research Papers
Meaning of in Design-by-Analysis Fatigue Evaluation
Gerry C. Slagis
e-mail: slagisg@asme.org
Gerry C. Slagis
G C Slagis Associates
, 258 Hillcrest Place, Pleasant Hill, California 94523
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Gerry C. Slagis
G C Slagis Associates
, 258 Hillcrest Place, Pleasant Hill, California 94523e-mail: slagisg@asme.org
J. Pressure Vessel Technol. Feb 2006, 128(1): 8-16 (9 pages)
Published Online: October 26, 2005
Article history
Received:
September 9, 2005
Revised:
October 26, 2005
Citation
Slagis, G. C. (October 26, 2005). "Meaning of in Design-by-Analysis Fatigue Evaluation." ASME. J. Pressure Vessel Technol. February 2006; 128(1): 8–16. https://doi.org/10.1115/1.2140798
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