A procedure is developed for determining the stress intensity factors in cracked polygonal plates. The method uses eigenfunctions of angular regions and satisfies the boundary conditions exactly. Westergaard's stress functions are used to satisfy the boundary conditions at the crack. Numerical resul
Calculation of stress intensity factors by efficient integration of weight functions
โ Scribed by A.A. Moftakhar; G. Glinka
- Publisher
- Elsevier Science
- Year
- 1992
- Tongue
- English
- Weight
- 589 KB
- Volume
- 43
- Category
- Article
- ISSN
- 0013-7944
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โฆ Synopsis
A numerical technique for simple and efficient integration of weight functions is presented. The method enables the stress intensity factors to be calculated with the aid of a hand calculator for any non-linear stress distribution normal to the crack surfaces. The proposed integration routine is validated against accurate numerical and analytical solutions. i B, i' K* 4x. a) M,, A4r and IU~ s s: si u ut x Xi XT e(x) ai c(X) c,(a) NOMENCLATURE crack length coefficients of the linearized stress function in the sub-interval '7" stress intensity factor stress intensity factor corresponding to the integral interval, 0.95 < u < 1.0 weight function parameters of the weight function area under the monotonic curve m(x, a) area under the linearized stress function u(x) corresponding to the sub-interval "i" area under the weight function curve m(x, a) corresponding to the sub-interval "7 normalized coordinate coordinate u of the centroid of the area St corresponding to the sub-interval "i" coordinate x of the centroid of the area S. coordinate x of the centroid of the area S, corresponding to the sub-interval "7 coordinate x of the centroid of the area St corresponding to the sub-interval "i" stress distribution value of stress function at x = xi value of stress function at x =X value of stress function at u = ui
๐ SIMILAR VOLUMES
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## Ab&aet -A simple representation for the crack-face disp~cement is emptoyed to compute a weight function soiely from stress intensity factors for a reference loading con~tion. Crack face disputants given by the represe&&n are shown to be in good agreement with analytical resub for cracked tensil
## At&r&-A finite element method with virtual crack extension technique is employed to find the weight function of the stress intensity factor for a cracked composite laminate. Since the weight function is load independent, once it is obtained, the stress intensity factor of a cracked laminate sub
Thermal shock stress intensity factor for an edge-cracked plate subjected to thermal shock is obtained from Bueckner's weight function method. It is shown that thermal shock stress intensity factor has maximum values with variation of time and crack length and that there is a critical crack length.