Life Prediction for Turbine Engine Components

Author:

Nicholas T.,Larsen J. M.

Publisher

Springer US

Reference18 articles.

1. “Analysis of Life Prediction Methods for Time-Dependent Fatigue Crack Initiation in Nickel-Base Superalloys,” National Materials Advisory Board, Publication NMAB-347, National Academy of Sciences, Washington, D.C., 1980.

2. Cruse, T. A. and Meyer, T. G., “Structural Life Prediction and Analysis Technology,” Air Force Aero Propulsion Laboratory Report AFAPL-TR-78-106, Wright-Patterson AFB, OH, 1978.

3. Hill, R. J., Reimann, W. H., and Ogg, J. S., “A Retirement-for-Cause Study of an Engine Turbine Disk,” Unpublished Air Force Wright Aeronautical Laboratories Report.

4. Harris, J. A., Jr., Sims, D. L., and Annis, C. G., Jr., “Concept Definition: Retirement for Cause of F100 Rotor Components,” Air Force Wright Aeronautical Laboratories Report, AFWAL-TR-80-4118, Wright-Patterson AFB, OH, 1980.

5. Duggan, T. B., “Philosophy of Safe Life Design,” Department of Mechanical Engineers, Portsmouth Polytechnic, Portsmouth, England, Unpublished Report, 1980.

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