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TECHNICAL PAPERS

On the Characterization of Fatigue Crack Growth in a Plate With a Single-Sided Repair

[+] Author and Article Information
C. N. Duong

The Boeing Company, 5301 Bolsa Avenue, MC H013-A316, Huntington Beach, CA 92647-2099

C. H. Wang

Defence Science & Technology Organization, 506 Lorimer Street, Fishermans Bend 3207, Australia

J. Eng. Mater. Technol 126(2), 192-198 (Mar 18, 2004) (7 pages) doi:10.1115/1.1647129 History: Received May 12, 2003; Revised September 26, 2003; Online March 18, 2004
Copyright © 2004 by ASME
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References

Figures

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Two-stage analytical procedure for determining the stress intensity factor in a plate with a single-sided repair: (a) the original problem; (b) stage I analysis; and (c) stage II analysis
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da/dN versus ΔKeff for Al 7075-T6 3.175 mm thick sheet
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da/dN versus ΔKeff for Al 7075-T6 1.27 mm thick sheet
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Analytical predictions versus test results of crack growth in specimen configuration 1
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Analytical predictions versus test results of crack growth in specimen configuration 2
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Analytical predictions versus test results of crack growth in specimen configuration 3
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Analytical predictions versus test results of crack growth in specimen configuration 4
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Analytical predictions versus test results of crack growth in specimen configuration 5. Since the relative humidity condition (RH) in this particular test varies quite significantly from one specimen to another, RH condition of the specimen is also indicated in the figure’s legend with low and high meaning low and high value of RH.
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Analytical predictions versus test results of crack growth in specimen configuration 6
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Analytical predictions versus test results of crack growth in specimen configuration 7
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Analytical predictions versus test results of crack growth in specimen configuration 8
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Analytical predictions versus test results of crack growth in specimen configuration 9

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