The interactive effects of high- and low-cycle loading on crack growth were evaluated for a high-temperature engine disk alloy (Inconel 718) over a wide range of low-cycle hold times, low-cycle stress intensity factor range (ΔK), high-cycle ΔK, and high-cycle frequency up to 1825 Hz. A series of fatigue crack growth experiments were carried out with a constant low-cycle ΔK and an increasing high-cycle ΔK. The high-frequency ΔK and crack length were measured with sufficient precision to capture details of the transition from the low-cycle dominated regime to the high-cycle dominated regime. In these experiments, the low- and high-cycle dominated growth regimes remained distinct over the entire range of low cycle ΔK, low cycle hold time and frequency investigated. An interactive effect apparent in the low-cycle dominated regime, was a retardation of the low-cycle growth rate when high-cycle loading was applied. The degree of retardation varied with low-cycle ΔK and frequency.
Skip Nav Destination
Article navigation
July 1986
This article was originally published in
Journal of Vibration, Acoustics, Stress, and Reliability in Design
Research Papers
The Influence of Several Combined High/Low Cycle Loading Parameters on the Crack Growth of a Turbine Disk Alloy
A. Petrovich,
A. Petrovich
Mechanical Technology Inc., Latham, NY
Search for other works by this author on:
W. Ziegler
W. Ziegler
Mechanical Technology Inc., Latham, NY
Search for other works by this author on:
A. Petrovich
Mechanical Technology Inc., Latham, NY
W. Ziegler
Mechanical Technology Inc., Latham, NY
J. Vib., Acoust., Stress, and Reliab. Jul 1986, 108(3): 262-267 (6 pages)
Published Online: July 1, 1986
Article history
Received:
July 1, 1985
Online:
November 23, 2009
Citation
Petrovich, A., and Ziegler, W. (July 1, 1986). "The Influence of Several Combined High/Low Cycle Loading Parameters on the Crack Growth of a Turbine Disk Alloy." ASME. J. Vib., Acoust., Stress, and Reliab. July 1986; 108(3): 262–267. https://doi.org/10.1115/1.3269337
Download citation file:
7
Views
0
Citations
Get Email Alerts
Cited By
Flexural wave propagation in rigid elastic combined metabeam
J. Vib. Acoust
Subband Decomposition Based Output-only Modal Analysis
J. Vib. Acoust
Related Articles
Fatigue Crack Growth Behavior Evaluation of Grainex Mar-M 247 for NASA’s High Temperature High Speed Turbine Seal Test Rig
J. Eng. Gas Turbines Power (March,2009)
Proposed New Fatigue Design Curves for Carbon and Low-Alloy Steels in High Temperature Water
J. Pressure Vessel Technol (April,2009)
Fatigue Crack Growth Behavior of Four Structural Alloys in High Temperature High Purity Oxygenated Water
J. Eng. Mater. Technol (July,1979)
Fatigue Life Prediction Modeling for Turbine Hot Section Materials
J. Eng. Gas Turbines Power (April,1989)
Related Proceedings Papers
Related Chapters
Control and Operational Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Fatigue Crack Growth, Fatigue, and Stress Corrosion Crack Growth: Section XI Evaluation
Online Companion Guide to the ASME Boiler and Pressure Vessel Codes