AIrstrati-The thermal stress intensity factors for interface cracks of Griffith and symmetric lip cusp types under vertical uniform heat flow in a finite body are calculated by the boundary element method. The boundary conditions on the crack surfaces are insulated or fixed to constant temperature.
Boundary element analysis of stress intensity factors for bimaterial interface cracks
โ Scribed by Kang Yong Lee; Hyung Jip Choi
- Publisher
- Elsevier Science
- Year
- 1988
- Tongue
- English
- Weight
- 769 KB
- Volume
- 29
- Category
- Article
- ISSN
- 0013-7944
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โฆ Synopsis
The stress intensity factors for bimaterial interface cracks are determined by the boundary element method employing the multi-region technique and the double-point concept. A formula relating the stress intensity factors to the crack surface displacement, which is applicable to both the homogeneous and the bimaterial systems, is derived. The accuracy of the numerical results obtained using the formula is shown to be satisfactory within 5% when compared with the pre-existing analytic solutions. The stress intensity factors for the edgecracked and the center-cracked bimaterial plates are computed with various crack lengths and shear modulus ratios under the biaxial and the uniaxial loadings, respectively.
๐ SIMILAR VOLUMES
The stress intensity factors of an interface crack in dissimilar materials are clarified and an extrapolation method to determine the stress intensity factors of an interface crack is proposed. The BEM using Hetenyi's fundamental solution is applied to crack problems in dissimilar materials and vari
At&m&--In case that the body with a cusp crack is under uniform heat Bow, thermal stress intensity factors are calculated by using the boundary element method with a linearized body force term, The crack surface is under an insulated or fixed temperature condition and the types of cracks are symmetr
oo13-7944/91 53.00 + 0.00 F'rinted in Great Britain.
The complex stress intensity factors for edge cracks located at the interface between fiber and matrix of a unidirectional graphite/epoxy laminate model subjected to a transverse tensile strain have been computed using the boundary element method. Such cracks might be generated due to a stress singu