An analytical model for flutter behavior of composite panels with shape memory alloy fibers
An analytical model for predicting the effect of shape memory alloys (SMA) on the flutter behavior of composite panels is developed in the frequency and time domains. The laminated plate theory and piston theory are employed to model the aeroelastic response of the composite panels to aerodynamic lo...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
JVE International
2016-06-01
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| Series: | Journal of Vibroengineering |
| Subjects: | |
| Online Access: | https://www.jvejournals.com/article/16771 |