Effect of age condition on fatigue properties of 2E12 aluminum alloy

Author:

Yan Liang,Du Feng-shan,Dai Sheng-long,Yang Shou-jie

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference20 articles.

1. GOLDEN P J, GRANDT A F, BRAY G H. A comparison of fatigue crack formation at holes in 2024-T3 and 2524-T3 aluminum alloy specimens [J]. International Journal of Fatigue, 1999, 21(1): S211–S219.

2. BRAY G H, BUCCI R J, COLVIN E L, KULAK M. Effect of prior corrosion on the S/N fatigue performance of aluminum sheet alloys 2024-T3 and 2524-T3 [J]. ASTM Special Technical Publication, 1997, 1298: 89–103.

3. WILLIAM C, JOHN L, JAMES T. Aluminum alloys for aircraft structure [J]. Advanced Materials and Processes, 2002, 160(12): 27–29.

4. IAU J, KULAK M. A new paradigm in the design of aluminum alloys for aerospace applications [J]. Materials Science Forum, 2000, 331/337: 127–140.

5. STARKE E A, STALEYT J T. Application of modern aluminum alloys to aircraft [J]. Progress in Aerospace Sciences, 1996, 32(2/3): 131–172.

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