FEM Modelling of the Heating Behaviour in Vibrothermography Based on Thermoelastic Damping on Crack Location

Choosak Ngaongam; Rapee  Ujjin

doi:10.37934/arfmts.108.1.6674

Authors

Choosak Ngaongam Department of Aviation Maintenance Engineering, College of Engineering, Rangsit University, Pathum Thani 12000, Thailand
Rapee Ujjin Department of Aviation Maintenance Engineering, College of Engineering, Rangsit University, Pathum Thani 12000, Thailand

DOI:

https://doi.org/10.37934/arfmts.108.1.6674

Keywords:

Thermoelastic damping, vibrothermography, surface crack, Non-destructive testing (NDT), aircraft material, vibrational frequency

Abstract

The paper aims to simulate the heat generation in crack location based on vibrothermography inspection. For this study, the thermoelastic damping effect was considered as the source of heat generation and the value of thermoelastic damping was determined. In simulation, the model of the specimen with crack was AL7075-T6. The vibrational frequencies were given at 20kHz, 24kHz and 28kHz, while the maximum amplitude was constant of 4.8nm. The results of temperature variation, stress, energy loss and heat flow rate on the crack location were obtained from the simulations which were performed by using ANSYS software. The ratio between power loss and heat flow rate was calculated and presented as the index for selecting the most suitable vibrational frequency in term of heat accumulation. The case study 20kHz was considered as the most suitable vibrational frequency for this study because the index ratio was higher than the case studies 24kHz, 28kHz at 6.29% and 9.14% respectively.