Microstructure and surface finish influences on AA7085-T7452 small fatigue crack growth rates

Author:

Main BenORCID,Dixon Ben,Jones Michael,Barter Simon

Funder

Defence Science and Technology Group

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference41 articles.

1. T, Mueller, L, Suffredini, D, Bush, R, Sawtell, P, Brouwer, “Alcoa Green Letter - Alcoa 7085 Die Forgings, 7th Generation Structural Solutions, 3rd Edition,” August 2006.

2. New generation high strength high damage tolerance 7085 thick alloy product with low quench sensitivity;Chakrabarti,2004

3. R. J. Bucci, H. Sklyut, L. Mueller, M. A. James, D. L. Ball, and J. K. Donald, “Advances in Testing and Analytical Simulation Methodologies to Support Design and Structural Integrity Assessment of Large Monolithic Parts: A New Perspective”. Presented at ASIP Conference 2005. [Online]. Available: http://www.asipcon.com/proceedings/proceedings_2005/ASIP_2005.pdf.

4. An overview of high-performance aircraft structural Al Alloy-AA7085;Prabhu;Acta Metallurgica Sinica (English Lett.),2015

5. K. Rendigs and M. Niedzinski, “Airbus and Current Aircraft Metal Technologies, Materials and Processes”, Airbus Germany GmbH, Bremen.

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