Numerical simulation of fatigue crack growth in steel-aluminium transition joint

PROCEEDINGS OF THE INTERNATIONAL CONFERENCE OF COMPUTATIONAL METHODS IN SCIENCES AND ENGINEERING 2019 (ICCMSE-2019) Pub Date : 2019-12-10 DOI:10.1063/1.5138099

M. Kowalski, D. Rozumek

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引用次数: 2

Abstract

The paper presents the results of fatigue crack growth simulation of the transition joint for S235JR steel and A5083 aluminum with the Grade 1 titanium interlayer coat and A1050 aluminum. Calculations were performed using ANSYS software. The publication presents the crack growth phenomena observed during fatigue testing. Additionally, calculations of residual stresses distributions induced by the process of joining materials during welding were carried out. Results of crack length calculations were comparable with experimantal data.The paper presents the results of fatigue crack growth simulation of the transition joint for S235JR steel and A5083 aluminum with the Grade 1 titanium interlayer coat and A1050 aluminum. Calculations were performed using ANSYS software. The publication presents the crack growth phenomena observed during fatigue testing. Additionally, calculations of residual stresses distributions induced by the process of joining materials during welding were carried out. Results of crack length calculations were comparable with experimantal data.

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钢-铝过渡接头疲劳裂纹扩展数值模拟

本文介绍了S235JR钢与A5083铝在层间包覆一级钛和A1050铝的过渡接头疲劳裂纹扩展的模拟结果。采用ANSYS软件进行计算。该出版物介绍了疲劳试验中观察到的裂纹扩展现象。此外，还对焊接过程中材料连接过程引起的残余应力分布进行了计算。裂缝长度计算结果与实验数据基本一致。本文介绍了S235JR钢与A5083铝在层间包覆一级钛和A1050铝的过渡接头疲劳裂纹扩展的模拟结果。采用ANSYS软件进行计算。该出版物介绍了疲劳试验中观察到的裂纹扩展现象。此外，还对焊接过程中材料连接过程引起的残余应力分布进行了计算。裂缝长度计算结果与实验数据基本一致。

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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来源期刊

PROCEEDINGS OF THE INTERNATIONAL CONFERENCE OF COMPUTATIONAL METHODS IN SCIENCES AND ENGINEERING 2019 (ICCMSE-2019)

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