An assessment of the role of near-threshold crack growth in high-cycle-fatigue life prediction of aerospace titanium alloys under turbine engine spectra

Author:

Larsen J. M.,Worth B. D.,Annis C. G.,Haake F. K.

Publisher

Springer Science and Business Media LLC

Subject

Mechanics of Materials,Modeling and Simulation,Computational Mechanics

Reference27 articles.

1. U.S. Air Force, Engine Structural Integrity Program, Military Standard 1783, Aeronautical Systems Division, Wright-Patterson Air Force Base, OH, 1984.

2. T. Nicholas and J.R. Zuiker, On the use of the Goodman diagram for high cycle fatigue design, International Journal of Fracture 80 (1996) 219–235.

3. B.A. Cowles, High cycle fatigue in aircraft gas turbines — an industry perspective, International Journal of Fracture 80 (1996) 147–163.

4. G.E. Dieter, Mechanical Metallurgy, Second Edition, McGraw Hill, New York (1976) 435–438.

5. U.S. Air Force Technical Report WRDC-TR-89-4085;F.K. Haake,1989

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