The Application of DIC Technique to Evaluate Residual Tensile Strength of Aluminum Alloy Plates with Multi-Site Damage of Collinear and Non-Collinear Cracks

This paper introduces an aviation industrial application of digital image correlation (DIC) technique on the measurement of residual tensile strength (RTS). In order to investigate multi-site damage (MSD) that is common in the fuselage of aging aircraft, RTS of 2024-T4 aluminum alloy sheet with MSD...

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Main Authors: Yajun Chen, Chunming Ji, Changtian Zhang, Shengjie Sun
Format: Article
Language:English
Published: MDPI AG 2019-01-01
Series:Metals
Subjects:
Online Access:https://www.mdpi.com/2075-4701/9/2/118
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spelling doaj-38dbaf09568d41f3a83d32732c4b8c162020-11-24T23:21:23ZengMDPI AGMetals2075-47012019-01-019211810.3390/met9020118met9020118The Application of DIC Technique to Evaluate Residual Tensile Strength of Aluminum Alloy Plates with Multi-Site Damage of Collinear and Non-Collinear CracksYajun Chen0Chunming Ji1Changtian Zhang2Shengjie Sun3Sino-European Institute of Aviation Engineering, Civil Aviation University of China, Tianjin 300300, ChinaSino-European Institute of Aviation Engineering, Civil Aviation University of China, Tianjin 300300, ChinaSino-European Institute of Aviation Engineering, Civil Aviation University of China, Tianjin 300300, ChinaBeijing Ruituo Technology Co., Ltd, Beijing 100020, ChinaThis paper introduces an aviation industrial application of digital image correlation (DIC) technique on the measurement of residual tensile strength (RTS). In order to investigate multi-site damage (MSD) that is common in the fuselage of aging aircraft, RTS of 2024-T4 aluminum alloy sheet with MSD was evaluated using DIC technique. Firstly, the four-factor and three-level orthogonal experiment was designed to optimize the DIC method to control the strain calculation error by considering subset size, interpolation tap, calibration score and step size. Secondly, RTS and strain fields were generated to analyze the path of crack propagation. The results show the optimal factor combination is 0.018 of calibration score, 23 pixels of subset size, step size is 1/4 of subset size and the filter size of interpolation calibration is 8 pixels. With the increase of spacing between adjacent holes, the RTS increases and the collinear cracked specimen becomes more perilous than that of non-collinear cracked while the hole spacing is 25 mm from the statistical analysis. Based on the Net section yield criterion, the RTS was calculated, which can give a conservative prediction of RTS.https://www.mdpi.com/2075-4701/9/2/118digital image correlationmulti-site damageresidual tensile strengthstrain calculation precision
collection DOAJ
language English
format Article
sources DOAJ
author Yajun Chen
Chunming Ji
Changtian Zhang
Shengjie Sun
spellingShingle Yajun Chen
Chunming Ji
Changtian Zhang
Shengjie Sun
The Application of DIC Technique to Evaluate Residual Tensile Strength of Aluminum Alloy Plates with Multi-Site Damage of Collinear and Non-Collinear Cracks
Metals
digital image correlation
multi-site damage
residual tensile strength
strain calculation precision
author_facet Yajun Chen
Chunming Ji
Changtian Zhang
Shengjie Sun
author_sort Yajun Chen
title The Application of DIC Technique to Evaluate Residual Tensile Strength of Aluminum Alloy Plates with Multi-Site Damage of Collinear and Non-Collinear Cracks
title_short The Application of DIC Technique to Evaluate Residual Tensile Strength of Aluminum Alloy Plates with Multi-Site Damage of Collinear and Non-Collinear Cracks
title_full The Application of DIC Technique to Evaluate Residual Tensile Strength of Aluminum Alloy Plates with Multi-Site Damage of Collinear and Non-Collinear Cracks
title_fullStr The Application of DIC Technique to Evaluate Residual Tensile Strength of Aluminum Alloy Plates with Multi-Site Damage of Collinear and Non-Collinear Cracks
title_full_unstemmed The Application of DIC Technique to Evaluate Residual Tensile Strength of Aluminum Alloy Plates with Multi-Site Damage of Collinear and Non-Collinear Cracks
title_sort application of dic technique to evaluate residual tensile strength of aluminum alloy plates with multi-site damage of collinear and non-collinear cracks
publisher MDPI AG
series Metals
issn 2075-4701
publishDate 2019-01-01
description This paper introduces an aviation industrial application of digital image correlation (DIC) technique on the measurement of residual tensile strength (RTS). In order to investigate multi-site damage (MSD) that is common in the fuselage of aging aircraft, RTS of 2024-T4 aluminum alloy sheet with MSD was evaluated using DIC technique. Firstly, the four-factor and three-level orthogonal experiment was designed to optimize the DIC method to control the strain calculation error by considering subset size, interpolation tap, calibration score and step size. Secondly, RTS and strain fields were generated to analyze the path of crack propagation. The results show the optimal factor combination is 0.018 of calibration score, 23 pixels of subset size, step size is 1/4 of subset size and the filter size of interpolation calibration is 8 pixels. With the increase of spacing between adjacent holes, the RTS increases and the collinear cracked specimen becomes more perilous than that of non-collinear cracked while the hole spacing is 25 mm from the statistical analysis. Based on the Net section yield criterion, the RTS was calculated, which can give a conservative prediction of RTS.
topic digital image correlation
multi-site damage
residual tensile strength
strain calculation precision
url https://www.mdpi.com/2075-4701/9/2/118
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