Subcritical crack growth behavior in Alloy 718 was studied at 425°C under static, cyclic, and combined loads. The results are analyzed using linear elastic fracture mechanics. Crack growth was shown to be cycle-dependent at all stress intensities at this temperature and hold times up to 10 min have no effect on the crack growth rates. On the other hand, crack growth is shown to occur readily under static loads at stress intensities less than half of the fracture toughness value. Comparison of the present results with those published in the literature showed that while crack growth is cycle-dependent at 425°C and time-dependent at 650°C, at an intermediate temperature, 540°C, it is time-dependent at low stress intensities and cycle-dependent at high stress intensities. Extrapolation of the present data shows that crack growth under static load could occur at temperatures above approximately 350°C and this may be a limiting factor for Alloy 718 for some of its high temperature applications.
Skip Nav Destination
Article navigation
October 1978
Research Papers
Crack Growth Behavior in Alloy 718 at 425°C
K. Sadananda,
K. Sadananda
Thermostructural Materials Branch, Engineering Materials Division, Naval Research Laboratory, Washington, D.C.
Search for other works by this author on:
P. Shahinian
P. Shahinian
Thermostructural Materials Branch, Engineering Materials Division, Naval Research Laboratory, Washington, D.C.
Search for other works by this author on:
K. Sadananda
Thermostructural Materials Branch, Engineering Materials Division, Naval Research Laboratory, Washington, D.C.
P. Shahinian
Thermostructural Materials Branch, Engineering Materials Division, Naval Research Laboratory, Washington, D.C.
J. Eng. Mater. Technol. Oct 1978, 100(4): 381-387 (7 pages)
Published Online: October 1, 1978
Article history
Received:
December 14, 1977
Revised:
February 13, 1978
Online:
August 17, 2010
Citation
Sadananda, K., and Shahinian, P. (October 1, 1978). "Crack Growth Behavior in Alloy 718 at 425°C." ASME. J. Eng. Mater. Technol. October 1978; 100(4): 381–387. https://doi.org/10.1115/1.3443507
Download citation file:
Get Email Alerts
Study on the Bending Behaviors of a Novel Flexible Re-entrant Honeycomb
J. Eng. Mater. Technol
The Fiftieth Anniversary of the Founding of the ASME Journal of Engineering Materials and Technology
J. Eng. Mater. Technol (July 2023)
Fatigue Damage Study of Steel–Aluminum Friction Stir Welding Joints Based on Equivalent Damage Model
J. Eng. Mater. Technol (October 2023)
Related Articles
A Review Paper on Aging Effects in Alloy 617 for Gen IV Nuclear Reactor Applications
J. Pressure Vessel Technol (April,2009)
Fatigue Crack Growth Behavior of Alloy 800H at Elevated Temperature
J. Eng. Mater. Technol (July,1991)
Experimental Characterization of Crack Tip Deformation Fields in Alloy 718 at High Temperatures
J. Eng. Mater. Technol (January,1998)
Related Proceedings Papers
Related Chapters
Applications of Elastic-Plastic Fracture Mechanics in Section XI, ASME Code Evaluations
Online Companion Guide to the ASME Boiler and Pressure Vessel Codes
Section III: Subsections NC and ND — Class 2 and 3 Components
Companion Guide to the ASME Boiler and Pressure Vessel Code, Volume 1, Fourth Edition
Control and Operational Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential