The role of threshold fatigue crack growth in life prediction of the alloy Ti-6Al-2Sn-4Zr-6Mo under high cycle fatigue spectra

American Society of Mechanical Engineers, Aerospace Division (Publication) AD

Volumn 55, Issue , 1997, Pages 443-448

  Larsen, James M ^a   Russ, Stephan M ^a   Maxwell, David C ^b   Worth, Brian D ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b UNIVERSITY OF DAYTON RESEARCH INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; CRACK PROPAGATION; FRACTURE MECHANICS; GAS TURBINES; RESIDUAL STRESSES; TITANIUM ALLOYS;

DAMAGE TOLERANCE METHODS; HIGH CYCLE FATIGUE (HCF);

FATIGUE OF MATERIALS;

EID: 0031387144     PISSN: 07334230     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (18)

1. ASTM E-647-95a, 1997, Standard Test Method for Measurement of Fatigue Crack Growth Rates," 1997 Annual Book of ASTM Standards, Vol. 03.01, ASTM, Philadelphia, PA, pp. 557-593.
2. Cowles, B. A., 1996, "High Cycle Fatigue in Aircraft Gas Turbines - An Industry Perspective," International Journal of Fracture, Vol. 80, pp. 147-163.
3. Haake, F. K., Salivar, G. C. Salivar, Kindle, E. H., Fischer, J. W., and Annis, C. G., Jr., 1989, "Threshold Fatigue Crack Growth Behavior," U. S. Air Force Technical Report WRDC-TR-89-4085, Wright-Patterson Air Force Base, OH.
4. Jira, J. R., Weerasooriya, T., Nicholas, T., and Larsen, J. M., 1988, "Effects of Closure on the Fatigue Crack Growth of Small Surface Cracks in a High-Strength Titanium Alloy," Mechanics of Fatigue Crack Closure, ASTM STP 982, J. C. Newman, Jr. and W. Elber, ed., American Society for Testing and Materials, Philadelphia, pp. 617-635.
5. Jira, J. R., Nicholas, T., and Larsen, J. M., 1987, "Fatigue Thresholds in Surface Flaws in Ti-6Al-2Sn-4Zr-6Mo," Fatigue 87, Vol. IV, E. Starke and R. O. Ritchie, ed., Engineering Materials Advisory Services, Ltd., West Midlands, U. K., pp. 1851-1860.
6. Kitagawa, H. and Takahashi, S., 1976, "Applicability of Fracture Mechanics to Very Small Cracks or the Cracks in the Early Stage," Proceedings of the Second International Conference on Mechanical Behavior of Materials, Boston, MA, pp. 627-631.
7. Larsen, J. M. and Jira, J. R., March 1991, "Small-Crack Closure Measurements in Titanium Alloys," Experimental Mechanics, pp. 82-87.
8. Larsen, J. M., Jira, J. R., and Weerasooriya, T., 1988, "Crack Opening Displacement Measurements on Small Cracks in Fatigue," Fracture Mechanics: Eighteenth Symposium, ASTM STP 945, D. T. Read and R. P. Reed, ed., American Society for Testing and Materials, Philadelphia, PA, pp. 896-912.
9. Larsen, J. M., Worth, B. D. Worth, Annis, C. G., Jr., and Haake, F. K., 1996, "An Assessment of the Role of Near-Threshold Crack Growth in High-Cycle-Fatigue Life Prediction of Aerospace Titanium Alloys Under Turbine Engine Spectra," International Journal of Fracture, Vol. 80, pp. 237-255.
10. Maxwell, D. C. and Nicholas, T., 1997, "A Rapid Method for Generation of a Haigh Diagram for High Cycle Fatigue," submitted for publication, ASTM STP, National Symposium on Fatigue and Fracture, American Society for Testing and Materials, Philadelphia, PA.
11. McDowell, D. L., 1996, "Basic Issues in the Mechanics of High Cycle Metal Fatiguè," International Journal of Fracture, Vol. 80, pp. 103-145.
12. Miller, K. J. and de los Rios, E. R., 1992, Short Fatigue Cracks, Mechanical Engineering Publications Limited, London, UK.
13. Nicholas, T. and Zuiker, J. R., 1996, "On the Use of the Goodman Diagram for High Cycle Fatigue Design," International Journal of Fracture, Vol. 80, pp. 219-235.
14. Ritchie, R. O. and Lankford, J., eds., 1986, Small Fatigue Cracks, The Minerals, Metals, and Materials Society, Warrendale, PA.
15. G. P. Sendeckyj, 1997, "History of Constant Life Diagrams," to be published in High Cycle Fatigue of Structural Materials: Paul C. Paris Symposium, TMS/ASM International, Warrendale, PA.
16. Taylor, D. and Knott, J. F., 1981, "Fatigue Crack Propagation Behaviour of Short Cracks; The Effect of Microstructure," Fatigue of Engineering Materials and Structures, Vol. 4, No. 2, pp. 147-155.
17. U.S. Air Force, Engine Structural Integrity Program., 1984, Military Standard 1783, Aeronautical Systems Division, Wright-Patterson Air Force Base, OH.
18. Zuiker, J. R. and Nicholas, T., 1996 "Observations and Limitations of the Use of The Goodman Diagram for Combined HCF/LCF Loading," FATIGUE '96, Elsevier Science Ltd., Oxford, U.K., pp. 467-472.