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...
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| Format: | article |
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2024
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| Online Access: | https://hdl.handle.net/11073/25822 |
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