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Elastodynamic analysis of the Finite punch and finite crack problems in orthotropic materials

机译:正交各向异性材料中有限冲头和有限裂纹问题的弹性动力学分析

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The transient elastodynamic response of the finite punch and finite crack problems in orthotropic materials is examined. Solution for the stress intensity factor history around the punch corner and crack tip is found. Laplace and Fourier transforms together with the Wiener-Hopf technique are employed to solve the equations of motion in terms of displacements. A detailed analysis is made in the simplified case when a flat rigid punch indents an elastic orthotropic half-plane, the punch approaches with a constant velocity normally to the boundary of the half-plane. An asymptotic expression for the singular stress near the punch corner is analyzed leading to an explicit expression for the dynamic stress intensity factor which is valid for the time the dilatational wave takes to travel twice the punch width. In the crack problem, a finite crack is considered in an infinite orthotropic plane. The crack faces are loaded by impact uniform pressure in mode. I an expression for the dynamic stress intensity factor is found which is valid while the dilatational wave travels the crack length twice. Results for orthotropic materials are shown to converge to known solutions for isotropic materials derived independently.
机译:研究了正交异性材料中有限冲头和有限裂纹问题的瞬态弹性动力学响应。找到了冲压角和裂纹尖端附近的应力强度因子历史的解。拉普拉斯(Laplace)和傅立叶(Fourier)变换与维纳-霍夫(Wiener-Hopf)技术一起用于解决位移方面的运动方程。在简化的情况下,当一个扁平的刚性冲头凹进一个弹性正交各向异性的半平面时,将进行详细的分析,该冲头通常以恒定的速度逼近该半平面的边界。分析了冲头拐角附近的奇异应力的渐近表达式,从而得到了动态应力强度因子的显式表达式,该表达式对于膨胀波传播两倍于冲头宽度所需的时间有效。在裂纹问题中,在无限正交各向异性平面中考虑了有限裂纹。裂纹面在冲击均匀压力下加载。我发现了一个动态应力强度因子的表达式,该表达式在膨胀波传播裂纹长度两次时是有效的。正交各向异性材料的结果显示收敛于独立导出的各向同性材料的已知解。

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