Experimental Evaluation of the Effective Electromechanical Coupling of a Vibrating Aircraft-Type Hybrid Honeycomb Sandwich Panel With Bonded Piezoelectric d31 Macro-Fibre Composite (MFC) Patch
This work presents the experimental evaluation challenges of the modal effective Electro-Mechanical Coupling Coefficient (EMCC) of a hybrid sandwich plate, made of regular (hexagonal) Aluminium honeycomb core and woven glass fibre-reinforced polymer composite faces, on which is bonded a piezoelectri...
Saved in:
| Main Author: | |
|---|---|
| Format: | article |
| Published: |
2024
|
| Subjects: | |
| Online Access: | https://hdl.handle.net/11073/25822 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Be the first to leave a comment!