Detecting and Monitoring Cracks in Aerospace Materials Using Post-Processing of TSA and AE Data



Middleton, Ceri A ORCID: 0000-0001-9488-9717, McCrory, John P, Greene, Richard J ORCID: 0000-0002-5373-0598, Holford, Karen and Patterson, Eann A ORCID: 0000-0003-4397-2160
(2019) Detecting and Monitoring Cracks in Aerospace Materials Using Post-Processing of TSA and AE Data. METALS, 9 (7). p. 748.

Access the full-text of this item by clicking on the Open Access link.
[img] Text
Middleton_et_el_2019_metals-09-00748.pdf - Published version

Download (1MB) | Preview

Abstract

<jats:p>Thermoelastic stress analysis (TSA) is a non-contact technique for measuring the distribution of stress in the surface of a component subject to cyclic loading by using a sensitive infrared camera. The stress concentrations indicative of a crack can be located and tracked using an optical flow method, allowing the position of the crack-tip to be identified at a given time. Acoustic emission (AE) has been used to validate the TSA algorithm. AE events from cracking, located using the Delta-T Mapping method, were detected several seconds before the TSA algorithm first detected cracking; however, TSA provided significantly more accurate location information.</jats:p>

Item Type: Article
Uncontrolled Keywords: thermoelastic stress analysis, acoustic emission, optical flow, Delta-T Mapping, crack tracking
Depositing User: Symplectic Admin
Date Deposited: 04 Jul 2019 07:20
Last Modified: 19 Jan 2023 00:38
DOI: 10.3390/met9070748
Open Access URL: https://www.mdpi.com/2075-4701/9/7/748
Related URLs:
URI: https://livrepository.liverpool.ac.uk/id/eprint/3048570