Title of article :
Methods for calculating stress intensity factors in anisotropic materials: Part I—z = 0 is a symmetric plane
Author/Authors :
Banks-Sills، نويسنده , , Leslie and Hershkovitz، نويسنده , , Itai and Wawrzynek، نويسنده , , Paul A. and Eliasi، نويسنده , , Rami and Ingraffea، نويسنده , , Anthony R.، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2005
Pages :
31
From page :
2328
To page :
2358
Abstract :
The problem of a crack in general anisotropic material under LEFM conditions is presented. In Part I, three methods are presented for calculating stress intensity factors for various anisotropic materials in which z = 0 is a plane of symmetry. All of the methods employ the displacement field obtained by means of the finite element method. The first one is known as displacement extrapolation and requires the values of the crack face displacements. The other two are conservative integrals based upon the J-integral. One employs symmetric and asymmetric fields to separate the mode I and II stress intensity factors. The second is the M-integral which also allows for calculation of KI and KII separately. these methods were originally presented for isotopic materials. Displacement extrapolation and the M-integral are extended for orthotropic and monoclinic materials, whereas the JI- and JII-integrals are only extended for orthotropic material in which the crack and material directions coincide. Results are obtained by these methods for several problems appearing in the literature. Good to excellent agreement is found in comparison to published values. New results are obtained for several problems. t II, the M-integral is extended for more general anisotropies. In these cases, three-dimensional problems must be solved, requiring a three-dimensional M-integral.
Keywords :
Anisotropic material , Stress intensity factors , Finite element method , Conservative integrals
Journal title :
ENGINEERING FRACTURE MECHANICS
Serial Year :
2005
Journal title :
ENGINEERING FRACTURE MECHANICS
Record number :
2341134
Link To Document :
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