Simulation of the Influence of Bonding Materials on the Dynamic Behavior of Laminated Composites

[+] Author and Article Information
Adnan H. Nayfeh

Air Force Material Laboratory, AFML/LLP, Wright Patterson AFB, Ohio 45433

Elsayed Abdel-Ati M. Nassar

Department of Aerospace Engineering and Applied Mechanics, University of Cincinnati, Cincinnati, Ohio 45221

J. Appl. Mech 45(4), 822-828 (Dec 01, 1978) (7 pages) doi:10.1115/1.3424426 History: Received January 01, 1978; Revised May 01, 1978; Online July 12, 2010


Two model analyses are constructed in order to determine the influence of bonding materials on the dynamic behavior of otherwise bilaminated composites. The geometric arrangement of the composite with the bond is treated as a special type of a trilaminated composite in which each of its major constituents is sandwiched between two bonding layers. In the first model, the recently developed continuum mixture theories of wave propagation in bilaminated composites [2] are extended to treat the trilaminated composite. Here details of the propagation process in the major components and also in the bonding layers are derived. In the second model, the entire effect of the bonds is treated as a modifier to interfacial continuity conditions. In this model the details of the propagation process in the bonding material are ignored. It is found that the results of both models correlate well for relatively thin bonding layers.

Copyright © 1978 by ASME
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