The details of the time history of the elastic waves in ballistically im pacted composite laminates have been obtained by using surface and em bedded strain gages. Records show that a very low-amplitude in-plane tensile wave arrives first followed by a medium-amplitude flexural wave and then a high-amplitude flexural wave. Measured and calculated values of wave speeds agree well.
Get full access to this article
View all access options for this article.
References
1.
N. Takeda and R.L. Sierakowski , "Localized Impact Problems of Composite Laminates " Shock and Vibration Digest (to be published).
2.
N. Takeda, R.L. Sierakowski and L.E. Malvern, "Experimental Impactor/Plate Configuration Interaction Studies of Impacted Glass Fiber-Reinforced Composite Laminates" submitted to SAMPE Quarterly.
3.
N. Takeda, R.L. Sierakowski and L.E. Malvern, "Transverse Cracks in Glass/Epoxy Cross-Ply Laminates Impacted by Projectiles," submitted to J. Materials Science .
4.
N. Takeda, R.L. Sierakowski and L.E. Malvern, "Microscopic Observations of Cross Sections of Impacted Composite Laminates," submitted to Composites.
5.
N. Takeda, R.L. Sierakowski and L.E. Malvern, "Delamination Crack Propagation Studies of Ballistically Impacted Composite Laminates" submitted to Experimental Mechanics .
6.
I.M. Daniel and T. Liber, "Wave Propagation in Fiber Composite Laminates" NASA CR-135086, July, 1976.
7.
P.F. Muldary, "Dynamics of Elastic Plates," M. S. Thesis, University of Minnesota, 1975.
8.
N. Takeda, "Experimental Studies of the Delamination Mechanisms in Impacted Fiber-Reinforced Composite Plates," Ph.D. Dissertation, University of Florida , 1980.