The high-cycle fatigue and fracture behavior of aluminum alloy 7055

Materials Science and Engineering: A

Volumn 281, Issue 1-2, 2000, Pages 292-304

  Srivatsan, T S ^a   Anand, S ^a   Sriram, S ^a   Vasudevan, V K ^b  

^a The University of Akron   (United States)

^b University of Cincinnati   (United States)

Author keywords

Aluminum alloy 7055; Deformation; Fatigue; Fracture behavior; Microstructure

Indexed keywords

BRITTLENESS; DEFORMATION; DUCTILITY; FATIGUE OF MATERIALS; FRACTURE TOUGHNESS; METALLOGRAPHIC MICROSTRUCTURE; STRESS ANALYSIS; THERMAL EFFECTS;

ALUMINUM ALLOY 7055;

ALUMINUM ALLOYS;

ALUMINUM ALLOY; DEFORMATION; FATIGUE; FRACTURE; MICROSTRUCTURE;

EID: 0034008485     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0921-5093(99)00716-9     Document Type: Article

References (43)

1. Staley J.T. "Aluminum-based products for the aerospace industry produced using non-traditional processing" First International Conference on Processing Materials for Properties, November 7-10, 1993, Honolulu, Hawaii, USA. 1994;The Minerals, Metals and Materials Society (TMS), Warrendale, PA, USA.
2. Staley J.T., Rolf R.L. International Symposium on Light Metals, August 1993. 1993;The Minerals, Metals and Materials Society (TMS), Warrendale, PA, USA.
3. Kaufman J.G. Design of aluminum alloys for high toughness and high fatigue strength. 40th Meeting of Structures and Materials Panel, NATO, Brussels, Belgium, April, 1975. 1975.
4. Sanders R.E. Jr, Starke E.A. Jr Met. Trans. 6A:1978;1087.
5. Hyatt M.V., Quist W.E. AFML Technical Report, TR-67-329. 1967.
6. Staley J.T. Technical Report. 1972;Naval Air Systems Command. Contract M00019-71-C-0131.
7. J.T. Staley, Microstructure and toughness of high strength aluminum alloys, presented at the ASTM Symposium on Properties as Related to Toughness, Montreal, Canada, June 1975.
8. Santner J.S. AFML Technical Report, TR-76-200. 1977;. March.
9. Ostermann F. Metall. Trans. 2:1971;2897-2902.
10. Starke E.A. Jr Mater. Sci. Eng. 29:1977;99-112.
11. DiRusso E., Conserva M., Gatto F., Markus H. Met. Trans. 4:1973;1133-1144.
12. Reimann W.H., Brisbane A.W. Eng. Fracture Mech. 5:1973;67-78.
13. Thompson D.S., Levy S.A., Benson D.K. Thermomechanical aging of aluminum alloys. Proceedings of the Third International Conference on Strength of Metals and Alloys, Cambridge, England. 1973;119-123.
14. Vruggink J.E. Technical Report, FA-TR 76-073. 1977;. April.
15. Sulinski H., Waldman J. Frankford Arsenal Summary Report. 1976;Frankford Arsenal, Philadelphia, PA. July.
16. Kuo V.W.C., Starke E.A. Jr Met. Trans. 16A:1985;1089-1099.
17. Starke E.A. Meshii M. Fatigue and Microstructure. 1979;405 American Society for Metals, Materials Park, OH.
18. Staley J.T. Jr Aluminum alloys and composites. Encylopedia of Physical Science. 1:1992;591-598.
19. Staley J.T., Lege D.J. J. Phys. IV. 3:1993;179-190.
20. Sanders T.H. Jr, Starke E.A. Jr Met. Trans. 7A:1976;1407.
21. Sanders R.E. Jr, Starke E.A. Jr Mater. Sci. Eng. 28:1977;53.
22. Fine M.E., Santner J.S. Scripta Met. 9:1975;1239.
23. Sanders T.H. Jr, Staley J.T. Meshii M. Fatigue and Microstructure. 1977;467 ASM International, Metals Park, OH.
24. Lutjering G., Doker H., Munz D. Microstructure and fatigue behavior of aluminum alloys: the microstructure and design of alloys. Proceedings of the Third International Conference on Strength of Metals and Alloys, Cambridge, England, August, 1973. 1973;427.
25. Viglione J. Evaluation of Size Effects on the Fatigue Properties of 7XXX-series Alloys. 1978;. NADC 72154, June.
26. Thompson D.S., Levy S.A., Spangler G.E. Fracture Toughness and Fatigue Resistance of Aluminum Sheet and Plate for Aircraft Applications, AFML TR-73-24211. 1973.
27. Brockenbrough J.R., Bucci R.J., Hinkle A.J., Magnusen P., Muyasato S.M. Role of Microstructure on Fatigue Durability of Aircraft Structural Alloys. 1993;. Final Report Office of Naval Research, Report No. ONR N00014-91-C-0128.
28. R.J. Bucci, Aluminum Company of America Report No. 57-77-24, Pittsburgh, PA, ALCOA Center, Pittsburgh, PA, USA, N79-32323, 1978.
29. Suresh S. Fatigue of Materials. second ed:1998;Cambridge University Press, London.
30. Srivatsan T.S. Int. J. Fatigue. 21:1999;557-569.
31. Staley J.T. Met. Trans. 5A:1974;929-940.
32. Standard E-8-93: Tension Testing of Metallic Materials. 1993;ASTM, Philadelphia, PA.
33. Standard E-466-82: Conducting Constant Amplitude Axial Fatigue Tests of Metallic Materials. 1995;ASTM, Philadelphia, PA.
34. Srivatsan T.S., Sriram S., Veeraraghavan D., Vasudevan V.K. J. Mater. Sci. 32:1997;2883-2894.
35. Srivatsan T.S., Anand S., Veeraraghavan D., Vasudevan V.K. J. Mater. Eng. Performance. 6(3):1997;349-359.
36. Fatigue and Fracture Handbook. 19:1996;ASM, Materials Park, OH.
37. Hornbogen E., Starke E.A. Jr Acta Met. Mater. 41(1):1993;1-16.
38. Geisler A.H. Trans. AIME. 180:1949;2456.
39. Thomas A.T. The Institute of Metals Conference on Modern Metallography in Metallurgy, Sheffield, England. 1968.
40. Welpmann K., Lutjering G., Bunk W. Aluminium. 50:1974;263.
41. Peters M., Lutjering G. Z. Metallkd. 67:1976;811.
42. Vasudevan A.K., Doherty R.D. Acta Met. 35(6):1987;1193-1219.
43. You C.P., Thompson A.W., Bernstein I.M. Met. Mater. Trans. A:1995;407. February.