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TECHNICAL PAPERS

Intensity of Singular Stress Fields at the End of a Cylindrical Inclusion

[+] Author and Article Information
N.-A. Noda, T. Genkai, Q. Wang

Mechanical Engineering Department, Kyushu Institute of Technology, Kitakyushu 804-8550, Japan

J. Appl. Mech 70(4), 487-495 (Aug 25, 2003) (9 pages) doi:10.1115/1.1598479 History: Received July 30, 1999; Revised January 16, 2003; Online August 25, 2003
Copyright © 2003 by ASME
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References

Figures

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Problem and coordinate system: (a) Uniaxial tension perpendicular to the axis of the inclusion (x direction); (b) Uniaxial tension in the axis of the inclusion (z direction); (c) Hydrostatic tension in a plane perpendicular to the axis of the inclusion (xy plane); (d) Pure shear in a plane perpendicular to the axis of the inclusion (xy plane); (e) Coordinate system
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Two types of body force distributed around the corner in the (a) normal, (b) tangential, and (c) circumferential directions
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(a) Typical boundary division for Eqs. (3) and (4). (b) Boundary division for singular integrals.
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FI,λ1 and FII,λ2 for a cylindrical inclusion (solid line) and a rectangular inclusion (broken line) under longitudinal tension (νMI=0.3)
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FI,λ1 and FII,λ2 for a cylindrical inclusion under uniaxial tension in the x direction (at corner A with θ=0, νMI=0.3)
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FI,λ1 and FII,λ2 for a cylindrical inclusion under uniaxial tension in the x direction (at corner A with θ=π/2, νMI=0.3)
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FI,λ1 and FII,λ2 for a rectangular inclusion under transverse tension, the case of plane strain νMI=0.3

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