Influence of Testing Frequency on Fatigue Crack Growth of 6061-T6 Aluminum Alloy in Hydrogen Gas Environment

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In order to investigate the effects of testing frequency on the fatigue crack growth rate of 6061-T6 aluminum alloy in hydrogen gas environment, fatigue crack growth tests were carried out on specimens with small artificial holes in 0.18 MPa hydrogen gas or in 0.18 MPa nitrogen gas. It takes long time to test at low testing frequency, so in this study an accelerated test method was proposed and fatigue tests were carried out using this method. The fatigue crack growth rate in hydrogen gas environment accelerates compared with in nitrogen gas environment. The crack growth rate at lower testing frequency tends to higher.

Info:

Periodical:

Key Engineering Materials (Volumes 353-358)

Edited by:

Yu Zhou, Shan-Tung Tu and Xishan Xie

Pages:

174-177

Citation:

A. Hagihara et al., "Influence of Testing Frequency on Fatigue Crack Growth of 6061-T6 Aluminum Alloy in Hydrogen Gas Environment", Key Engineering Materials, Vols. 353-358, pp. 174-177, 2007

Online since:

September 2007

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$38.00

[1] Special issue on recent advances in the engineering aspects of hydrogen embrittlement (Engineering Fracture Mechanics, 68-10 1988).

[2] P. J. Ferreia, I. M. Robertson and H. K. Birnbaum: Acta mater. Vol. 47, No. 10, (1999), p.2991.

[3] T. Ishikawa and R.B. McLellan: Acta metall. Vol. 34, No. 6, (1986), p.1091.