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Mode I crack tip fie1ds with incomplete crack tip plasticity in plane stress

机译:模式I裂纹尖端在平面应力中具有不完全的裂纹尖端可塑性

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The Mode I asymptotic crack tip stress field is developed for a plane stress stationary crack in an elastic--perfectly plastic solid. The crack tip sector configuration consists of a centered fan ahead of the crack tip and an elastic sector in the angular range 39.l26 ≤ θ≤ l80. The angular distributions of the crack tip stress field are continuous and the corresponding asymptotic deformation field is kinematically admissible. This crack tip stress field is verified by comparison with a small-scale yielding finite element solution. It is inferred from the finite element results that the in-plane components of the asymptotic strain field are continuous at all angles around the crack tip. Closed form empirical expressions are obtained for the amplitude functions which measure the strengths of the l/r strain singularity in the centered fan.
机译:模式I渐近裂纹尖端应力场是为弹性完全塑性固体中的平面应力固定裂纹而开发的。裂纹尖端扇形结构由裂纹尖端前面的中心风扇和39.126≤θ≤180°的角度范围内的弹性扇形组成。裂纹尖端应力场的角分布是连续的,相应的渐近形变场在运动学上是允许的。通过与小规模屈服有限元解比较,验证了该裂纹尖端应力场。从有限元结果可以推断,渐近应变场的平面内分量在裂纹尖端周围的所有角度都是连续的。对于幅度函数,获得了封闭形式的经验表达式,该函数测量了中心扇中l / r应变奇异性的强度。

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