Smart damping of a simply supported laminated CNT-based hybrid composite plate using FE approach

2022 ◽  
Vol 171 ◽  
pp. 108782
Author(s):  
Madhur Gupta ◽  
M.C. Ray ◽  
Nagesh D. Patil ◽  
S.I. Kundalwal
Keyword(s):  
Hybrid Composite ◽  
Composite Plate ◽  
Simply Supported ◽  
Hybrid Composite Plate

Dynamic Response of Smart Hybrid Composite Plate Subjected to Low-Velocity Impact

2007 ◽  
Vol 41 (19) ◽  
pp. 2347-2370 ◽  
Author(s):  
S.M.R. Khalili ◽  
A. Shokuhfar ◽  
F. Ashenai Ghasemi ◽  
K. Malekzadeh
Keyword(s):  
Dynamic Response ◽  
Hybrid Composite ◽  
Composite Plate ◽  
Low Velocity Impact ◽  
Low Velocity ◽  
Velocity Impact ◽  
Hybrid Composite Plate

Development of jute rope hybrid composite plate using carbon fibre

2015 ◽  
Vol 56 (6) ◽  
pp. 1095-1113 ◽  
Author(s):  
Karim Nouri ◽  
Md. Ashraful Alam ◽  
Mohammad Mohammadhassani ◽  
Mohd Zamin Bin Jumaat ◽  
Amir Hosein Abna
Keyword(s):  
Carbon Fibre ◽  
Hybrid Composite ◽  
Composite Plate ◽  
Hybrid Composite Plate

scholarly journals Identification of Modal Properties of Composite Thin Plate Using OMA in Wind Tunnel Environment

2013 ◽  
Vol 446-447 ◽  
pp. 606-610
Author(s):  
Z.A.C. Saffry ◽  
Dayang Laila Majid ◽  
Fairuz Izzuddin Romli ◽  
Faizal Mustapha ◽  
Ermira Junita Abdullah
Keyword(s):  
Wind Tunnel ◽  
Hybrid Composite ◽  
Composite Plate ◽  
Dynamic Properties ◽  
Research Work ◽  
Modal Testing ◽  
Structural Deformation ◽  
Modal Parameters ◽  
Laser Vibrometer ◽  
Hybrid Composite Plate

Identification of modal parameters is crucial especially in aerospace applications whereby the interactions of airflow with aircraft structures can result in undesirable structural deformations. This structural deformation can be predicted with knowledge of the modal parameters. This can be achieved through conventional modal testing that requires a known excitation force in order to extract these dynamic properties. This technique can be experimentally complex because of the need for artificial excitation and it also does not represent actual operational condition. The current work presents part of research work that address the practical implementation of operational modal analysis (OMA) applied to a cantilevered hybrid composite plate exposed to low speed airflow in a wind tunnel. A single contactless sensing system via a laser vibrometer is employed to measure the response. OMA technique applied in a wind-on condition succeeded in extracting the modal parameters of the hybrid composite plate which correlate well with modal testing using impact hammer excitation.

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