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功能梯度涂层III型界面裂纹的动应力强度因子

ynamic Stress Intensity Factor of Mode III Interface Crack of Functionally Graded Coating

中文摘要英文摘要

本文对功能梯度涂层—半无限大基体结构界面运动裂纹问题进行了研究。根据不同材料界面的连接条件,将问题中所有各量用单一未知函数表达。采用了材料剪切模量和密度函数的指数模型,通过Fourier积分变换方法推导了运动界面裂纹受到剪切载荷问题的对偶积分方程。利用Jacobi多项式将位移展开成级数形式,并采用Schmidt数值方法获得裂纹尖端的动应力强度因子的半解析解。分析了裂纹运动速度、梯度参数和涂层厚度对裂纹尖端应力场的影响。结果表明:裂纹尖端应力具有奇异性;梯度参数和涂层厚度越大,动应力强度因子越低;裂纹速度越大,动应力强度因子越大。增大功能梯度涂层厚度和梯度参数是降低界面裂纹的应力强度因子,可提高材料的安全性。

Research is conducted to investigate the moving crack on the interface between the functionally graded coating and infinite substrate structure with free boundary in this paper. Using the bonding conditions of the interface between different media, all the quantities in our question have been represented with a single unknown function, and the dual integral equation of moving crack problem is obtained through Fourier transform with the help of the exponent model of the shear modulus and density. The displacement is expanded into series form using Jacobi Polynomial by Schmidt method, then the semi-analytic and numerical solutions of dynamic stress intensity factor are derived. The influences of parameters such as crack velocity, graded parameter and coating height on dynamic stress intensity factor are also studied. The results show that the stress at the crack tip is of singularity; dynamic stress intensity factors decrease with the increasing graded parameter and coating height, increase with increasing of crack propagation rate for the problems of interface moving crack. Increasing graded parameter and coating height can be used to reduce the stress concentration and raise material security, so we can adjust dynamic stress intensity factor by changing the graded parameter and coating height.

李新刚、吕念春、王振清

力学材料科学

界面运动裂纹功能梯度涂层对偶积分方程Schmidt方法动应力强度因子

Interface moving crackFunctionally graded coatingDual integral equationsSchmidt methodynamic stress intensity factor

李新刚,吕念春,王振清.功能梯度涂层III型界面裂纹的动应力强度因子[EB/OL].(2009-02-20)[2025-08-16].http://www.paper.edu.cn/releasepaper/content/200902-1066.点此复制

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