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Stress-intensity factors for circumferential surface cracks in pipes and rods under tension and bending loadsThe purpose of this paper is to present stress-intensity factors for a wide range of nearly semi-elliptical surface cracks in pipes and rods. The configurations were subjected to either remote tension or bending loads. For pipes, the ratio of crack depth to crack length (a/c) ranged from 0.6 to 1; the ratio of crack depth to wall thickness (a/t) ranged from 0.2 to 0.8; and the ratio of internal radius to wall thickness (R/t) ranged from 1 to 10. For rods, the ratio of crack depth to crack length also ranged from 0.6 to 1; and the ratio of crack depth to rod diameter (a/D) ranged from 0.05 to 0.35. These particular crack configurations were chosen to cover the range of crack shapes (a/c) that have been observed in experiments conducted on pipes and rods under tension and bending fatigue loads. The stress-intensity factors were calculated by a three-dimensional finite-element method. The finite-element models employed singularity elements along the crack front and linear-strain elements elsewhere. The models had about 6500 degrees of freedom. The stress-intensity factors were evaluated using a nodal-force method.
Document ID
19850027111
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Raju, I. S.
(Analytical Services and Materials, Inc. Hampton, VA, United States)
Newman, J. C., Jr.
(NASA Langley Research Center)
Date Acquired
September 5, 2013
Publication Date
August 1, 1985
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-87594
NAS 1.15:87594
Report Number: NASA-TM-87594
Report Number: NAS 1.15:87594
Accession Number
85N35424
Funding Number(s)
PROJECT: RTOP 505-33-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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