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Application of the line-spring model to a cylindrical shell containing a circumferential or axial part-through crackAn approximate solution was obtained for a cylindrical shell containing a part-through surface crack. It was assumed that the shell contains a circumferential or axial semi-elliptic internal or external surface crack and was subjected to a uniform membrane loading or a uniform bending moment away from the crack region. A Reissner type theory was used to account for the effects of the transverse shear deformations. The stress intensity factor at the deepest penetration point of the crack was tabulated for bending and membrane loading by varying three dimensionless length parameters of the problem formed from the shell radius, the shell thickness, the crack length, and the crack depth. The upper bounds of the stress intensity factors are provided by the results of the elasticity solution obtained from the axisymmetric crack problem for the circumferential crack, and that found from the plane strain problem for a circular ring having a radial crack for the axial crack. The line-spring model gives the expected results in comparison with the elasticity solutions. Results also compare well with the existing finite element solution of the pressurized cylinder containing an internal semi-elliptic surface crack.
Document ID
19810011935
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Delale, F.
(Lehigh Univ. Bethlehem, PA, United States)
Erdogan, F.
(Lehigh Univ. Bethlehem, PA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1981
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-164058
Report Number: NASA-CR-164058
Accession Number
81N20464
Funding Number(s)
CONTRACT_GRANT: NSF CME-78-08737
CONTRACT_GRANT: NGR-39-007-011
CONTRACT_GRANT: DOT-RC-82007
CONTRACT_GRANT: NSF CME-78-08737
CONTRACT_GRANT: NGR-39-007-011
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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