On the free vibration behavior of Timoshenko sandwich beam model with honeycomb core and nano-composite face sheet layers integrated by sensor and actuator layers
European Physical Journal Plus, ISSN: 2190-5444, Vol: 137, Issue: 6
2022
- 6Citations
- 9Captures
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Example: if you select the 1-year option for an article published in 2019 and a metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019. If you select the 3-year option for the same article published in 2019 and the metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019, 2018 and 2017.
Citation Benchmarking is provided by Scopus and SciVal and is different from the metrics context provided by PlumX Metrics.
Article Description
In this research, the free vibration behavior of Timoshenko sandwich microbeam model is investigated. It is considered that this structure models with honeycomb core and nano-composite face sheet layers integrated by sensor and actuator layers. The governing equations of motion are obtained by applying the Hamilton’s principle based on modified couple stress theory. The numerical results are obtained by using Navier’s method and the effect of various parameters including volume fraction of CNT, temperature change, material length scale parameter, material type of sensor and actuator, material properties and geometric parameters of honeycomb core and geometric parameters of sandwich microbeam are illustrated.
Bibliographic Details
http://www.scopus.com/inward/record.url?partnerID=HzOxMe3b&scp=85133011548&origin=inward; http://dx.doi.org/10.1140/epjp/s13360-022-02896-0; https://link.springer.com/10.1140/epjp/s13360-022-02896-0; https://dx.doi.org/10.1140/epjp/s13360-022-02896-0; https://link.springer.com/article/10.1140/epjp/s13360-022-02896-0
Springer Science and Business Media LLC
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