Vibration of a laminated composite plate is controlled by passive and active control methods. Stiffness change in composite structures by changes in laminate orientation is used as an example of a passive control method, negative velocity feedback control with the piezoelectric sensor/actuator is us
β¦ LIBER β¦
Optimum placement of piezoelectric sensor/actuator for vibration control of laminated beams
β Scribed by Kang, Young K.; Park, Hyun C.; Hwang, Woonbong; Han, Kyung S.
- Book ID
- 121416453
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 1996
- Tongue
- English
- Weight
- 691 KB
- Volume
- 34
- Category
- Article
- ISSN
- 0001-1452
- DOI
- 10.2514/3.13326
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