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Book synopsis

The effect of different aging treatments on fatigue crack growth behavior ofAA6013 aluminum alloy was investigated. C(T) (Compact Tension) specimenswere prepared in L-T and T-L direction for fatigue crack growth tests. Sampleswere in T651 as received, T42 which is solution heat treated at 538 şC for 90minutes, water quenched and aged in room temperature for 96 hours, and onegroup of samples were overaged at 245 şC for 12 hours after T42 condition wasachieved. Hardness and conductivity measurements were achieved for allconditions after the heat treatments.Fatigue crack growth tests were performed at as received condition T651, T42and 245 şC aged samples in laboratory air with sinusoidal loading of stress ratioR=0.1 and at a frequency of 1 Hz. The highest fatigue crack growth resistance isobserved for T651 T-L and 245 şC overaged L-T condition.

Book details

Book category Books in English Technology, engineering, agriculture Technology: general issues Engineering: general

• Full title: Fatigue Crack Growth Behaviour of Aa6013 Aluminum Alloy
• Author: Aziz Egemen Varli
• Language: English
• Binding: Paperback
• Number of pages: 104
• EAN: 9783639129762
• ISBN: 3639129768
• ID: 06821724
• Publisher: VDM Verlag
• Weight: 163 g
• Dimensions: 229 × 152 × 6 mm
• Date of publishing: 05. March 2009

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