Influence of Dwell at Peak Load on Elevated Temperature Fatigue Crack Growth in Waspaloy

Author:

BYRNE J.,HALL R.

Publisher

Elsevier

Reference8 articles.

1. “The specification of Gas Turbine Disc Forgings”;Jeal;Metals and Materials,1985

2. “Cyclic Behaviour of Disc Alloys At 650°C”;Cowles;J Eng Mat Tech,1980

3. “Fatigue Crack Propagation of Nickel-Base Superalloys at 650°C”;Gayda,1988

4. Byrne, J, Hall, R, Alabraba, M, Grabowski, L and Hussey, I W (1991), “Elevated Temperature Fatigue Crack Growth in a Nickel Base Superalloy Under Dwell Conditions”, Proc 6th Int Conf Mech Behaviour of Mtls, Kyoto, vol 4,pp. pp. 361–36

5. ASTM (1983) “Standard Test Method for Constant-Load Amplitude Fatigue Crack Growth Rates Above 10−8m/cycle”, ASTM Standard E-647–83, Pt 3,pp. 710–730

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