FATIGUE BEHAVIOUR OF FIBRE METAL LAMINATE (GLARE) VIS-(A)-VIS PLAIN AEROSPACE ALUMINUM ALLOY:AN EXPERIMENTAL INVESTIGATION

摘要：

　　Performance of cracked fibre metal laminate (Glare) under fatigue load differs from that of cracked plain aerospace aluminum alloy.Load transfer towards stronger fibres in Glare shields crack tips in aluminum layers that retards fatigue crack growth rates.The paper experimentally investigates the fatigue behaviour of Glare at variable stress ratios in an ambient environment for comparison with that of plain aerospace aluminum alloy.

关键词： Crack growth rate Fatigue Fibre bridging Fibre metal laminate Glare Stress ratio

作者: Sunil Bhat

作者单位: School of Mechanical and Building Sciences, Vellore Institute of Technology, Vellore-632014, Tamil Nadu, India

会议类型: 国际会议

会议名称: 2012 International Conference on Engineering Materials,Geotechnical Engineering and Environmental Engineering(EMGEEE2012)(2012工程材料、岩石工程和环境工程国际会议)

会议地点: 石家庄

会议语种:英文

页码: 7-12

在线出版日期: 2012-10-26（万方平台首次上网日期，不代表论文的发表时间）