NASA NTRS · 19770004172
Wave propagation in fiber composite laminates, part 2
Abstract
An experimental investigation was conducted to determine the wave propagation characteristics, transient strains and residual properties in unidirectional and angle-ply boron/epoxy and graphite/epoxy laminates impacted with silicone rubber projectiles at velocities up to 250 MS-1. The predominant wave is flexural, propagating at different velocities in different directions. In general, measured wave velocities were higher than theoretically predicted values. The amplitude of the in-plane wave is less than ten percent of that of the flexural wave. Peak strains and strain rates in the transverse to the (outer) fiber direction are much higher than those in the direction of the fibers. The dynamics of impact were also studied with high speed photography.
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Daniel, I. M., Liber, T.. 1976-06-01. Wave propagation in fiber composite laminates, part 2. https://ntrs.nasa.gov/citations/19770004172
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