Experimental Study On Active Vibration Control Of Honeycomb Sandwich Plates
- Paper number
IAC-07-C2.5.10
- Author
Mr. Wang Jiang, Beijing Institute of Astronautical Systems Engineering, China
- Coauthor
Ms. Xu Weixiu, Beijing Institute of Astronautical Systems Engineering, China
- Coauthor
Ms. Tong Wenmin, Beijing Institute of Astronautical Systems Engineering, China
- Coauthor
Mr. Yang Zhiguang, Beijing Institute of Astronautical Systems Engineering, China
- Year
2007
- Abstract
The modes and natural frequencies of honeycomb plates are obtained by ANYSYS and experiences. On the base of the consistency of FEM analysis and experiences, piezoelectric sensors and actuators are installed at the positions where strains are largest. Experiences on active vibration control are carried out and effects on vibration suppression are outstanding.
- Abstract document
- Manuscript document
IAC-07-C2.5.10.pdf (🔒 authorized access only).
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