Crack growth rate da/dN in Alloy 718 at 650°C, compared on the conventional ΔK basis, increased with increase in R (Kmin/Kmax) and also generally with inclusion of hold time at Kmax and Kmin. An exception, however, was that a 1-min hold at a Kmin just below the threshold K for creep crack growth caused retardation of crack growth. Correlation of da/dN for various R levels was better with Kmax than with other parameters such as Kmin, ΔK, and Δ J-integral. Fatigue crack growth in the alloy was found to be time dependent and Kmax controlled under these test conditions and consequently the best overall correlation was given by da/dt with Kmax. An unusual observation was that the addition of hold time to the loading cycle at near zero Kmin (R = 0.05) caused an increase in da/dN, as the result of an environmental interaction.
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July 1979
Research Papers
Effects of Stress Ratio and Hold-Time on Fatigue Crack Growth in Alloy 718
P. Shahinian,
P. Shahinian
Thermostructural Materials Branch, Material Science and Technology Division, Naval Research Laboratory, Washington, D.C. 20375
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K. Sadananda
K. Sadananda
Thermostructural Materials Branch, Material Science and Technology Division, Naval Research Laboratory, Washington, D.C. 20375
Search for other works by this author on:
P. Shahinian
Thermostructural Materials Branch, Material Science and Technology Division, Naval Research Laboratory, Washington, D.C. 20375
K. Sadananda
Thermostructural Materials Branch, Material Science and Technology Division, Naval Research Laboratory, Washington, D.C. 20375
J. Eng. Mater. Technol. Jul 1979, 101(3): 224-230 (7 pages)
Published Online: July 1, 1979
Article history
Received:
January 1, 1979
Online:
August 17, 2010
Citation
Shahinian, P., and Sadananda, K. (July 1, 1979). "Effects of Stress Ratio and Hold-Time on Fatigue Crack Growth in Alloy 718." ASME. J. Eng. Mater. Technol. July 1979; 101(3): 224–230. https://doi.org/10.1115/1.3443681
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