Effects of process variables on fretting fatigue crack initiation in Ti-6Al-4V

Journal of Strain Analysis for Engineering Design

Volumn 37, Issue 6, 2002, Pages 535-547

  Namjoshi, S A ^a   Mall, S ^b   Jain, V K ^c   Jin, O ^a  

^a Air Force Institute of Technology   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c UNIVERSITY OF DAYTON   (United States)

Author keywords

Crack initiation; Critical plane based parameters; Fatigue; Fretting; Friction; Process volume; Titanium

Indexed keywords

CRACK INITIATION; FINITE ELEMENT METHOD; FRICTION; GRAIN SIZE AND SHAPE; PARAMETER ESTIMATION; SHEAR STRENGTH; TITANIUM ALLOYS;

FRETTING FATIGUE;

FATIGUE TESTING;

EID: 18744406983     PISSN: 03093247     EISSN: None     Source Type: Journal    
DOI: 10.1243/030932402320950143     Document Type: Conference Paper

References (24)

1. Hoeppner, D.W., Chandrasekaran, V. and Elliot, C.B. (Eds) Fretting-Fatigue: Current Technology and Practices, ASTM STP 1367, 2000 (American Society for Testing and Materials, West Conshohocken, Pennsylvania).
2. Rayaproula, D. and Cook, R. A critical review of fretting-fatigue investigations at the Royal Aerospace Establishment. In Standardizaton of Fretting-Fatigue Test Methods and Equipment, ASTM STP 1159 (Eds M. Helmi and R. Waterhouse), 1992, pp. 129-152 (American Society for Testing and Materials, West Conshohocken, Pennsylvania).
3. Lindley, T. and Nix, K. Fretting fatigue in the power generation industry: experiments, analysis, and integrity assessment. In Standardizaton of Fretting-Fatigue Test Methods and Equipment, ASTM STP 1159 (Eds M. Helmi and R. Waterhouse), 1992, pp. 153-169 (American Society for Testing and Materials, West Conshohocken, Pennsylvania).
4. Waterhouse, R. Fretting-fatigue. Int. Mater. Rev., 1992, 37(2), 77-97.
5. Cowles, A.B. High cycle fatigue in aircraft gas turbines - An industry perspective. Int. J. Fracture, 1996, 80, 147-163.
6. Nicholas, T. Critical issues in high cycle fatigue. Int. J. Fatigue, 1999, 21, S221-S231.
7. Krgo, A., Kallmeyer, A.R. and Kurath, P. Evaluation of HCF multiaxial fatigue life prediction methodologies for Ti-6Al-4V. In Proceeding of the 5th National Turbine Engine High Cycle Fatigue Conference, Chandler, Arizona, 7-9 March 2000.
8. Smith, R.N., Watson, P. and Topper, T.H. A stress-strain function for the fatigue of metals. J. Mater., JMLSA, 1970, 5, 767-778.
9. Findley, W.N. Fatigue of metals under combinations of stresses. Trans. ASME, 1957, 79, 1337-1348.
10. Fatemi, A. and Socie, D. A critical plane approach to multiaxial fatigue damage including out of phase loading. Fatigue and Fracture of Engng Mater. Structs, 1988, 11, 149-165.
11. Namjoshi, S.A., Mall, S., Jain, V.K. and Jin, O. Fretting fatigue crack initiation mechanism in Ti-6Al-4V. Fatigue and Fracture of Engng Mater. Structs (in press).
12. Dang Van, K. Macro-Micro approach in high-cycle multiaxial fatigue. In Advances in Multiaxial Fatigue, ASTM STP 1191 (Eds D.L. McDowell and R. Ellis), 1993, pp. 120-130 (American Society for Testing and Materials, West Conshohocken, Pennsylvania).
13. Fouvry, S., Kapsa, P. and Vincent, L. A multiaxial fatigue analysis of fretting contact taking into account the size effect. In Fretting-Fatigue: Current Technology and Practices, ASTM STP 1367 (Eds D.W. Hoeppner, V. Chandrasekaran and C.B. Elliot), 1999, pp. 167-182 (American Society for Testing and Materials, West Conshohocken, Pennsylvania).
14. Lamacq, V., Dubourg, M. and Vincent, L. A theoretical model for the prediction of initial growth angles and sites of fretting fatigue cracks. Tribology Int., 1997, 30(6), 391-400.
15. Mura, T. and Nakasone, Y. A theory of fatigue crack initiation in solids. J. Appl. Mechanics, 1990, 57, 1-6.
16. Slavik, D.C., Dunyak, T., Griffiths, J. and Kurath, P. Crack initiation modeling in Ti-6Al-4V for smooth and notched geometries. In Proceedings of the 5th National Turbine Engine High Cycle Fatigue Conference, Chandler, Arizona, 7-9 March 2000.
17. Swalla, D.R. and Neu, R.W. Characterization of fretting fatigue process volume using finite element analysis. In Fretting-Fatigue: Advances in Basic Understanding and Applications, STP 1425 (Eds Y. Mutoh, S.E. Kinyon and D.H. Hoeppner), (American Society for Testing and Materials, West Conshohocken, Pennsylvania) (in press).
18. Lykins, C.D., Mall, S. and Jain, V.K. An evaluation of parameters for predicting fretting fatigue crack initiation. Int. J. Fatigue, 2000, 20, 703-716.
19. Lykins, C.D., Mall, S. and Jain, V.K. Combined experimental-numerical investigation of fretting fatigue crack initiation. Int. J. Fatigue, 2001, 23, 703-711.
20. Lykins, C.D., Mall, S. and Jain, V.K. A shear stress based parameter for fretting fatigue crack initiation. Fatigue and Fracture of Engng Mater. Structs, 2001, 24, 461-473.
21. Iyer, K. and Mall, S. Analysis of contact pressure and stress amplitude effects on fretting fatigue life. Trans. ASME, J. Engng Mater. Technol., 2001, 123(1), 85-93.
22. Tsai, C.T. and Mall, S. Elasto-plastic finite element analysis of fretting stresses in pre-stressed strip in contact with cylindrical pad. Finite Elements in Analysis and Des., 2000, 36, 171-187.
23. Walker, K. The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7075-T6 aluminum. In Effects of Environment and Complex Load History on Fatigue Life, STP 462, 1970, pp. 1-14 (American Society for Testing and Materials, Philadelphia, Pennsylvania).
24. ABAQUS Standard Users Manual, 1995 (Hibbit, Karlsson and Sorensen, Providence, Rhode Island).