Abstract
This paper deals with optimal design of sandwich composite laminates consisting of high- stiffness and expensive surface and low-stiffness and inexpensive core layers. The
objective is to determine ply angles and number of core layers in such a way that natural frequency is maximized with minimal material cost. A Genetic Algorithm (GA) procedure is
used for simultaneous cost minimization and frequency maximization. The proposed model is applied to a graphiteepoxy/ glass-epoxy laminate and results are obtained for various
aspect ratios and number of layers.
objective is to determine ply angles and number of core layers in such a way that natural frequency is maximized with minimal material cost. A Genetic Algorithm (GA) procedure is
used for simultaneous cost minimization and frequency maximization. The proposed model is applied to a graphiteepoxy/ glass-epoxy laminate and results are obtained for various
aspect ratios and number of layers.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of ICMPM, International Conference on Advances in Materials, Product Design and Manufacturing Systems |
| Number of pages | 5 |
| Publication date | 2005 |
| Publication status | Published - 2005 |
| Externally published | Yes |
| Event | International Conference on Advances in Materials, Product Design and Manufacturing Systems - Sathyamangalam, India Duration: 12 Dec 2005 → 14 Dec 2005 |
Conference
| Conference | International Conference on Advances in Materials, Product Design and Manufacturing Systems |
|---|---|
| Country/Territory | India |
| City | Sathyamangalam |
| Period | 12/12/2005 → 14/12/2005 |
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