International Journal of Vehicle Structures and Systems

Open Access Open Access  Restricted Access Subscription Access

Infra-Red Thermography Based Inspection of Hybrid Composite Laminates under Flexure Loading


Affiliations
1 Dept. of Aeronautical Engg., Tagore Engineering College, Chennai, Tamilnadu, India
2 Dept. of Aeronautical Engg., Bharath Institute of Higher Education and Research, Tamilnadu, India
 

   Subscribe/Renew Journal


Generally, the aircraft structural parts are economically high in cost so the materials need to be inspected for defects or damages using various non-destructive testing (NDT) methods like ultrasonic, thermography and acoustic emission. The aim of this project is to characterize the defects in composite laminates before and after the flexural loading using infra-red thermography NDT method. GFRP and hybrid (GFRP+CFRP) composite laminates are fabricated with different orientation such as uni-directional, cross ply, anti-symmetric and angle ply and then tested under flexural loading according to ASTM D790 standard. The volume fraction of the fibre and matrix needs to be found out to know the void content and the mixing ratio of reinforcement and binder.

Keywords

Glass Fibre Reinforced Plastic, Flexural Test, Delamination, Infra-Red Thermography, Non-Destructive Testing.
User
Subscription Login to verify subscription
Notifications
Font Size

Abstract Views: 244

PDF Views: 124




  • Infra-Red Thermography Based Inspection of Hybrid Composite Laminates under Flexure Loading

Abstract Views: 244  |  PDF Views: 124

Authors

R. Bhoominathan
Dept. of Aeronautical Engg., Tagore Engineering College, Chennai, Tamilnadu, India
P. Divyabarathi
Dept. of Aeronautical Engg., Bharath Institute of Higher Education and Research, Tamilnadu, India
R. Manimegalai
Dept. of Aeronautical Engg., Tagore Engineering College, Chennai, Tamilnadu, India
T. Nithya
Dept. of Aeronautical Engg., Tagore Engineering College, Chennai, Tamilnadu, India
S. Shanmugapriya
Dept. of Aeronautical Engg., Tagore Engineering College, Chennai, Tamilnadu, India

Abstract


Generally, the aircraft structural parts are economically high in cost so the materials need to be inspected for defects or damages using various non-destructive testing (NDT) methods like ultrasonic, thermography and acoustic emission. The aim of this project is to characterize the defects in composite laminates before and after the flexural loading using infra-red thermography NDT method. GFRP and hybrid (GFRP+CFRP) composite laminates are fabricated with different orientation such as uni-directional, cross ply, anti-symmetric and angle ply and then tested under flexural loading according to ASTM D790 standard. The volume fraction of the fibre and matrix needs to be found out to know the void content and the mixing ratio of reinforcement and binder.

Keywords


Glass Fibre Reinforced Plastic, Flexural Test, Delamination, Infra-Red Thermography, Non-Destructive Testing.



DOI: https://doi.org/10.4273/ijvss.10.1.02