Abstract
The purpose of this study is to investigate experimentally the fatigue crack growth behavior under typical service loading spectrum recorded from military P-3 cargo airplane. The material is 2324 — T39 Al alloy widely used in the aircraft industry. Experiments were conducted using the full spectrum and modified versions of it such as only ‘positive’ (no negative loads) or with reduced (clipped) high peaks. The results show that the compressive loads decrease fatigue life of the specimen by ~300%. Furthermore, by running tests with clipped peaks it was found that the fatigue life was shorten significantly due to reduction of crack growth retardation caused by highest tensile peaks. Multiple tests were conducted in order to establish a scatter in the experimental data under spectrum loads.
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References
L. Anderson, Fracture Mechanics: Fundamentals and Applications, 3rd edition, 2006, CRC Press LLC, Boca Raton, FL.
S. Suresh, Fatigue of Metals, 2nd edition, Cambridge University Press, Cambridge, 1998.
N.E. Dowling, Mechanical Behavior of Materials: Engineering Methods for Deformation, Fracture and Fatigue, 3rd edition,, Prentice-Hall, Upper Saddle River, NJ, 2006.
S. Stoychev and D. Kujawski, Analysis of crack propagation using ΔK and Kmax, International Journal of Fatigue, Vol. 27, 2005, pp. 1425–1431.
ASTM E 647-05 “Standard Test Method for Measurement of Fatigue Crack Growth”, Annual Book of ASTM Standards, Vol. 03.01, 2006, American Society For Testing and Materials, West Conshohocken, PA.
H. Tada, P.C. Paris and G.R. Irwin, The Stress Analysis for Cracks Handbook, 2nd edition, Paris Productions, St. Louis, MO, 1985.
J. Newman, Jr., Private communication, 2002.
J. Schijve and D. Broek, Crack propagation tests based on a Gust spectrum with variable amplitude loading, Aircraft Engineering, Vol. 34, 1962, pp. 314–316.
www.mae.wmich.edu/labs/Solid>Mechanics/experimental/spectrum_data/spectrum_data.html
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© 2009 Springer Science+Business Media B.V
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Kujawski, D., Stoychev, S. (2009). Fatigue Crack Growth Behavior under Spectrum Loading. In: Pantelakis, S., Rodopoulos, C. (eds) Engineering Against Fracture. Springer, Dordrecht. https://doi.org/10.1007/978-1-4020-9402-6_18
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DOI: https://doi.org/10.1007/978-1-4020-9402-6_18
Publisher Name: Springer, Dordrecht
Print ISBN: 978-1-4020-9401-9
Online ISBN: 978-1-4020-9402-6
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