Evaluation of Interfacial Fracture Toughness of a Bi-Material System Under Thermal Loading Conditions

Jianjun Wang, D. Zou, Sheng Liu
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Abstract

In this paper, the interfacial fracture toughness of a bi-material (molding compound/silicon) specimen subjected to a series of thermal loads was evaluated using a high density laser moiré interferometry coupled with FEA technique. The moiré interferometry technique was used to monitor and measure the crack length during the test. A finite element technique was simultaneously used to determine the near crack tip displacement fields of the bi-material specimen. The interfacial fracture toughness and phase angle were computed by using these near tip displacement variables through the analytical energy release rate and phase angle expressions derived by authors. The results show that the interfacial fracture toughness of the bi-material specimen considered is strongly related to the phase angle in terms of the defined phase angle expression in this paper. The interfacial fracture toughness Gc and the phase angle ϕ of the tested bi-material specimen at the interface corresponding to the crack length a = 3.0mm under the temperature rise thermal load from room temperature (20° C) to 120° C are 13.64 J/m and −54.28° respectively, while the interfacial fracture toughness Gc and the phase angle ϕ of the tested bi-material specimen at the interface of the molding compound/silicon with the crack length a = 3.3mm under the temperature rise thermal load from room temperature (20° C) to 138° C are 20.02 J/m2 and −54.8° respectively.
热载荷条件下双材料体系界面断裂韧性的评价
本文采用高密度激光干涉法结合有限元分析技术,对双材料(模塑复合材料/硅)试样在一系列热载荷作用下的界面断裂韧性进行了评价。在试验过程中,采用涡流干涉法对裂纹长度进行了监测和测量。同时采用有限元方法确定了双材料试样的近裂纹尖端位移场。利用这些近尖端位移变量,通过作者导出的解析能量释放率和相角表达式,计算界面断裂韧性和相角。结果表明,根据本文定义的相角表达式,所考虑的双材料试样的界面断裂韧性与相角密切相关。在室温(20℃)至120℃的温升热载荷作用下,双材料试样在裂纹长度a = 3.0mm处的界面断裂韧性Gc和相位角φ分别为13.64 J/m和- 54.28°;在室温(20℃)至138℃的温升热载荷下,裂纹长度为a = 3.3mm的复合材料/硅的界面断裂韧性Gc和相位角φ分别为20.02 J/m2和- 54.8°。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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