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TECHNICAL PAPERS

Statistical Considerations in the Analysis of Data From Fatigue Tests on Delaminated Cross-Ply Graphite/Epoxy Composites

[+] Author and Article Information
Valeria La Saponara, George A. Kardomateas

School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30332-0150

J. Eng. Mater. Technol 122(4), 409-414 (Apr 15, 2000) (6 pages) doi:10.1115/1.1289287 History: Received January 24, 2000; Revised April 15, 2000
Copyright © 2000 by ASME
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References

Figures

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Specimen’s geometry (dimensions are in mm)
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Buckling of the specimen under loading
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First branching in specimen 10 (Table 1)
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Second and third branching in specimen 10 (Table 1)
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First branching in specimen 10
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Second and third branching in specimen 10
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Absolute value of the kink angle (in deg) versus the log10 of the number of cycles. Zero branching angle is included. m=mean STD=standard deviation.
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Absolute value of the kink angle (in deg) versus the log10 of the number of cycles. Zero branching is not included in the calculations. m=mean, STD=standard deviation.
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Median of normalized crack length versus the median of the absolute value of branching angles, for Sequence 1. ○=3R smoother, * =raw data.
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Median of normalized crack length versus the median of the absolute value of branching angles, for Sequence 2. ○=3R smoother, * =raw data.

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