Experimental study of fretting crack nucleation in aerospace alloys with emphasis on life prediction

ASTM Special Technical Publication

Volumn , Issue 1367, 2000, Pages 267-281

  Szolwinski, M P ^a   Harish, G ^b   McVeigh, P A ^b   Farris, T N ^b  

^a RENSSELAER POLYTECHNIC INSTITUTE   (United States)

^b Purdue University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; ALUMINUM ALLOYS; CRACK PROPAGATION; FAILURE ANALYSIS; FATIGUE TESTING; FINITE ELEMENT METHOD; FRETTING CORROSION; INTERFACES (MATERIALS); JOINTS (STRUCTURAL COMPONENTS); MATHEMATICAL MODELS; RESIDUAL STRESSES; STRESS ANALYSIS;

AEROSPACE ALLOYS; CRACK NUCLEATION; FRETTING FATIGUE; RIVETED LAP JOINTS;

FATIGUE OF MATERIALS;

EID: 0033879191     PISSN: 10403094     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1520/stp14735s     Document Type: Conference Paper

References (24)

1. Farris, T. N., Szolwinski, M. P., and Harish, G., "Fretting in Aerospace Structures and Materials," Fretting Fatigue: Current Technology and Practices, ASTM STP 1367, D. W. Hoeppner, V. Chandrasekaran, and C. B. Elliott, Eds., American Society for Testing and Materials, West Conshohocken, PA, 1999.
2. Harris, W. J., Metallic Fatigue, Pergamon Press, New York, NY, 1961.
3. Heywood, R. B., Designing Against the Fatigue of Metals, Jarrold and Sons, Norwich, Great Britain, 1962.
4. Piascik, R. S. and Willard, S. A., "The Characteristics of Fatigue Damage in the Fuselage Riveted Lap Splice Joint," NASA/TP-97-206257, NASA Langley Research Center, Hampton, VA, 1997.
5. Fawaz, S. A., "Fatigue Crack Growth in Riveted Joints," Ph.D. Thesis, Delft University, The Netherlands, 1997.
6. Hoeppner, D. W., Elliot, C. B., III, and Moesser, M. W., "The Role of Fretting Fatigue on Aircraft Rivet Hole Cracking," DOT/FAA/AR-96/10, Federal Aviation Administration, Salt Lake City, UT, 1996.
7. Harish, G., Szolwinski, M. P., and Farris, T. N., "Finite Element Modeling of Rivet Installation and Riveted Joints for Prediction of Fretting Crack Nucleation," in Joint DoD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah, USA, 1997, pp. 647-663.
8. Harish, G. and Farris, T. N., "Effect of Fretting Contact Stresses on Crack Nucleation in Riveted Lapjoints," in A Collection of Technical Papers, Proceedings of 39th AIAA/ASME/ASCE Structures, Structural Dynamics and Materials Conference, Long Beach, CA, 1998, pp. 383-391.
9. Szolwinski, M. P. and Farris, T. N., "Observation, Analysis and Prediction of Fretting Fatigue in 2024-T351 Aluminum Alloy," Wear, Vol. 221, No. 1, 1998, pp. 24-36.
10. Nowell, D. and Hills, D. A., "Crack Initiation Criteria in Fretting Fatigue," Wear, Vol. 136, 1990, pp. 329-343.
11. MIL-HDBK-5G, Metallic Material and Elements for Aerospace Vehicle Structures, Vol. 1, Defense Printing Service Detachment Office, Philadelphia, PA, 1994.
12. McVeigh, P. A. and Farris, T. N., "Finite Element Analysis of Fretting Stresses," Journal of Tribology, Vol. 119, No. 4, 1997, pp. 797-801.
13. Fouvry, S., Kapsa, P., Vincent, L., and Dang Van, K., "Theoretical Analysis of Fatigue Cracking Under Dry Friction for Fretting Loading Conditions," Wear, Vol. 195, 1996, pp. 21-34.
14. Szolwinski, M. P. and Farris, T. N., "Mechanics of Fretting Fatigue Crack Formation," Wear, Vol. 198, 1996, pp. 93-107.
15. Smith, K. N., Watson, P., and Topper, T. H., "A Stress-Strain Function for the Fatigue of Metals," Journal of Materials, Vol. 5, No. 4, 1970, pp. 767-778.
16. Socie, D., "Critical Plane Approaches for Multiaxial Fatigue Damage Assessment," Advances in Multiaxial Fatigue, ASTM STP 1191, D. L. McDowell and R. Ellis, Eds., American Society for Testing and Materials, Philadelphia, PA, 1993, pp. 7-36.
17. Bannantine, J. A., Comer, J. J., and Handrock, J. L., Fundamentals of Metal Fatigue Analysis, Prentice-Hall, Englewood Cliffs, NJ, 1990.
18. Hertzberg, R. W., Deformation and Fracture Mechanics of Engineering Materials, Wiley and Sons, New York, NY, 1976.
19. Blatt, P. A., "Evaluation of Fatigue Crack Initiation Behavior of An Experimental Ternary Aluminum-Lithium Alloy," Master's Thesis, Purdue University, West Lafayette, IN, 1990.
20. Szolwinski, M. P., "The Mechanics and Tribology of Fretting Fatigue With Application to Riveted Lap Joints," Ph.D., Purdue University, West Lafayette, IN, 1998.
21. Harish, G. and Farris, T. N., "Modeling of Skin/Rivet Contact: Application to Fretting Fatigue," in A Collection of Technical Papers, Proceedings of 38th AIAA/ASME/ASCE Structures, Structural Dynamics and Materials Conference, Volume 4, Kissimmee, FL, 1997, pp. 2761-2771.
22. Müller, R. P. G., "An Experimental and Analytical Investigation on the Fatigue Behavior of Fuselage Riveted Lap Joints," Ph.D., Delft University of Technology, The Netherlands, 1995.
23. Boller, C. and Seeger, T., Materials Data for Cyclic Loading, Part D: Aluminum and Titanium Alloys, Materials Science Monographs, C. Laird, Ed., Vol. 42D, Elsevier, Amsterdam, 1987.
24. Wang, H. L., Buhler, K., and Grandt, A. F., Jr., "Evaluation of Multiple Site Damage in Lap Joint Specimens," in 1995 USAF Structural Integrity Program Conference, San Antonio, TX, 1995, pp. 21-38.