E-11 FATIGUE BEHAVIOUR OF OIL JET PEENED ALUMINIUM ALLOY, AA 6063-T6(Session: Fatique/Contact Strength)

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概要

• 論文の詳細を見る

• Surface modification using oil jet peening is a recently developed process used for the introduction of compressive residual stresses. Aluminum alloy AA6063-T6 specimens were peened for different peening durations. Peening duration was found to affect the magnitude of residual stress and hardness. Fatigue life depends upon the on compressive residual stress as well as surface roughness of the peened parts.

• 一般社団法人日本機械学会の論文
• 2006-11-08

著者

• Gnanamoorthy R.

  Department Of Mechanical Engineering Indian Institute Of Technology Madras

• Sahaya Grinspan

  Department of Mechanical Engineering, Indian Institute of Technology Madras

• Sahaya Grinspan

  Department Of Mechanical Engineering Indian Institute Of Technology Madras

関連論文

• E-11 FATIGUE BEHAVIOUR OF OIL JET PEENED ALUMINIUM ALLOY, AA 6063-T6(Session: Fatique/Contact Strength)

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