Abstract
For ballistically impacted glass/epoxy cross-ply laminated plates with three five-layer unidirectional laminas, high-speed photos were taken from the back of plates, illuminated from the front side. The semitransparency of the plates enabled a Nova high-speed camera to record delamination-crack propagations at speeds of up to 40,000 frames/s. The delamination crack in the fiber direction of the first (second) lamina at the first (second) interface, propagated initially at 300–400 (400–500) m/s which decreased to 200–300 (270–400) m/s during the period of observation, and decelerated to a stop within 100 (300) μs. This last velocity range (270–400 m/s) agreed well with the largest-amplitude flexural-wave velocity measured by strain gages. This is a documentation that delamination is associated with the flexural wave.
A velocity gage consisting of a silver conductive paint was modified to measure propagation velocities of the generator strip which was cut from the first lamina by two through-the-thickness cracks and which initiated a sequential delamination. This generator-strip-formation velocity was higher than the measured delamination-crack-propagation velocity. This fact is consistent with the assumption that the generator strip initiates delamination cracks.
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References
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This research was conducted as part of the PhD dissertation while N. Takeda was Graduate Student, Department of Engineering Sciences, U. of F. from Sept. 1978 to Aug. 1980.
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Takeda, N., Sierakowski, R.L., Ross, C.A. et al. Delamination-crack propagation in ballistically impacted glass/epoxy composite laminates. Experimental Mechanics 22, 19–25 (1982). https://doi.org/10.1007/BF02325699
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DOI: https://doi.org/10.1007/BF02325699