Abstract
The characteristics of elastic waves emanating from crack initiation in 2024 and 5052 aluminum alloys subject to static and fatigue loading were investigated through laboratory experiments. The objective of the study was to determine the differences in the properties of the signals generated from static and fatigue tests and also to examine if the sources of the waves could be identified from the temporal and spectral characteristics of the acoustic emission waveforms. The signals were recorded using nonresonant, flat, broadband transducers attached to the surface of the alloy specimens. The time dependence and power spectra of the signals recorded during the tests were examined and classified according to their special features. Three distinct types of signals were observed. The waveforms and their power spectra were found to be dependent on the material and the type of fracture associated with the signals. Analysis of the waveforms indicated that some signals could be attributed to plastic deformation associated with static tests. The potential application of the approach in health monitoring of aging aircraft structures using a network of surface mounted broadband sensors is discussed.
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References
Aging of U.S. Air Force Aircraft, Publication NMAB-488-2 (National Academy Press, Washington, DC, 1997).
Annual Book of ASTM Standards, Section 3, “Metals Test Methods and Analytical Procedures,” Vol. 3: Nondestructive Testing (ASTM, Philadelphia, PA, 1993).
Acoustic Emission Testing, Nondestructive Testing Handbook Vol. 5 (ASNT, Columbus, OH, 1987).
S.H. Carpenter and M.R. Gorman, J. Acoustic Emission 13, 51 (1995).
D. Buttle and C. Scruby, J. Acoustic Emission 9, 243 (1990).
C. Heiple, S. Carpenter, and D. Armentrout, J. Acoustic Emission 10, 103 (1992).
S. McBride, J. Maclanchlan, and B. Paradis, J. of Nondestructive Evaluation 2, 35 (1981).
M. Friesel, Materials Evaluation No. 47, 28, 842 (1989).
C. Scala and S. Cusland, Mater. Sci. Eng. 76, 83 (1987).
I.M. Daniel, J.J. Luo, C.G. Sifniotopoulos, and H.J. Chun, Rev. Prog. Quan. Nondestr. Eval. 16, 451 (1997).
D. Guo, A.K. Mal, and K. Ono, J. Acoustic Emission 14, S19 (1996).
E. Haugse, T.J. Leeks, R. Ikegami, P.E. Johnson, S.M. Ziola, J.F. Doroghi, S. May, and N. Phelps, in Nondestructive Evaluation of Aging Aircraft, Airports, and Aerospace Hardware III, Bellingham, Washington, edited by A. Mal (Proc. SPIE 3586, 1999), pp. 32–40.
K-W. Nam, A.K. Mal, and R.P. Wei, in Proc. Third FAA/DOD/NASA Conference on Aging Aircraft, (Galaxy Scientific, Albuquerque, NM) Sept 20–23 (1999, in press).
J.U. Wu, Mater’s Thesis, University of California, Los Angeles, CA (1995).
S.L. McBride, J.M. Maclachlan, and B.P. Paradis, J. Nondestr. Eval. 2, 35 (1981).
S.H. Carpenter and F.P. Higgins, Metall. Trans. A 8A, 1629 (1977).
M.A. Hamstad, R. Bianchetti, and A.K. Mukherjee, Eng. Fract. Mech. 9, 663 (1977).
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Nam, K., Mal, A. Characteristics of elastic waves generated by crack initiation in aluminum alloys under fatigue loading. Journal of Materials Research 16, 1745–1751 (2001). https://doi.org/10.1557/JMR.2001.0241
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DOI: https://doi.org/10.1557/JMR.2001.0241