Reference-free damage detection, localization, and quantification in composites
In this study, a reference-free damage characterization technique is developed not only to identify but also to locate and quantify damage in composite structures subject to varying temperature conditions. First, damage is characterized in terms of a damage index (m-value) defined as the ratio of da...
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Published in | The Journal of the Acoustical Society of America Vol. 133; no. 6; pp. 3838 - 3845 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
United States
01.06.2013
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Online Access | Get full text |
ISSN | 0001-4966 1520-8524 1520-8524 |
DOI | 10.1121/1.4802744 |
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Abstract | In this study, a reference-free damage characterization technique is developed not only to identify but also to locate and quantify damage in composite structures subject to varying temperature conditions. First, damage is characterized in terms of a damage index (m-value) defined as the ratio of damage size to the wavelength of the A0 mode within the damage. Then, a feasible solution space defining all possible combinations of the damage location and size are estimated without using any prior baseline data obtained from the pristine condition of a structure or different paths. When additional information such as the A0 mode group velocity within the pristine region of the structure becomes available, the estimates for the damage location and size are updated with better accuracy. The uniqueness of this study lies in that damage localization and quantification as well as identification are all performed without comparing current Lamb wave signals with the ones obtained from the pristine condition of the target structure, making the proposed technique more attractive for online monitoring. Numerical and experimental tests are presented to demonstrate the effectiveness of the proposed damage detection technique under varying temperature. |
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AbstractList | In this study, a reference-free damage characterization technique is developed not only to identify but also to locate and quantify damage in composite structures subject to varying temperature conditions. First, damage is characterized in terms of a damage index (m-value) defined as the ratio of damage size to the wavelength of the A0 mode within the damage. Then, a feasible solution space defining all possible combinations of the damage location and size are estimated without using any prior baseline data obtained from the pristine condition of a structure or different paths. When additional information such as the A0 mode group velocity within the pristine region of the structure becomes available, the estimates for the damage location and size are updated with better accuracy. The uniqueness of this study lies in that damage localization and quantification as well as identification are all performed without comparing current Lamb wave signals with the ones obtained from the pristine condition of the target structure, making the proposed technique more attractive for online monitoring. Numerical and experimental tests are presented to demonstrate the effectiveness of the proposed damage detection technique under varying temperature. In this study, a reference-free damage characterization technique is developed not only to identify but also to locate and quantify damage in composite structures subject to varying temperature conditions. First, damage is characterized in terms of a damage index (m-value) defined as the ratio of damage size to the wavelength of the A0 mode within the damage. Then, a feasible solution space defining all possible combinations of the damage location and size are estimated without using any prior baseline data obtained from the pristine condition of a structure or different paths. When additional information such as the A0 mode group velocity within the pristine region of the structure becomes available, the estimates for the damage location and size are updated with better accuracy. The uniqueness of this study lies in that damage localization and quantification as well as identification are all performed without comparing current Lamb wave signals with the ones obtained from the pristine condition of the target structure, making the proposed technique more attractive for online monitoring. Numerical and experimental tests are presented to demonstrate the effectiveness of the proposed damage detection technique under varying temperature.In this study, a reference-free damage characterization technique is developed not only to identify but also to locate and quantify damage in composite structures subject to varying temperature conditions. First, damage is characterized in terms of a damage index (m-value) defined as the ratio of damage size to the wavelength of the A0 mode within the damage. Then, a feasible solution space defining all possible combinations of the damage location and size are estimated without using any prior baseline data obtained from the pristine condition of a structure or different paths. When additional information such as the A0 mode group velocity within the pristine region of the structure becomes available, the estimates for the damage location and size are updated with better accuracy. The uniqueness of this study lies in that damage localization and quantification as well as identification are all performed without comparing current Lamb wave signals with the ones obtained from the pristine condition of the target structure, making the proposed technique more attractive for online monitoring. Numerical and experimental tests are presented to demonstrate the effectiveness of the proposed damage detection technique under varying temperature. |
Author | Sohn, Hoon Jin Lim, Hyung Min Yeum, Chul Min Kim, Ji |
Author_xml | – sequence: 1 givenname: Hyung surname: Jin Lim fullname: Jin Lim, Hyung – sequence: 2 givenname: Hoon surname: Sohn fullname: Sohn, Hoon – sequence: 3 givenname: Chul surname: Min Yeum fullname: Min Yeum, Chul – sequence: 4 givenname: Ji surname: Min Kim fullname: Min Kim, Ji |
BackLink | https://www.ncbi.nlm.nih.gov/pubmed/23742338$$D View this record in MEDLINE/PubMed |
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Cites_doi | 10.1016/j.jsv.2006.10.044 10.1109/TUFFC.2009.1357 10.1016/j.jsv.2009.03.014 10.1016/j.compscitech.2011.04.011 10.1109/78.258082 10.1088/0964-1726/15/6/028 10.1088/0964-1726/13/1/017 10.1016/j.compstruct.2004.02.013 10.1016/S0041-624X(02)00136-1 10.1088/0964-1726/14/6/001 10.1016/j.ultras.2005.05.001 10.1088/0964-1726/18/8/085011 10.1121/1.3533741 10.1016/S0022-460X(02)01193-8 10.1088/0964-1726/16/6/042 10.1016/0041-624X(96)00024-8 10.1088/0957-0233/16/5/024 10.1177/073168449301200504 10.1088/0964-1726/17/01/015007 10.1016/j.wavemoti.2011.01.001 10.1088/0964-1726/19/6/065009 10.1016/j.ndteint.2011.08.003 10.1121/1.407495 10.1177/0021998305052021 10.1016/S0041-624X(98)00012-2 10.1088/0964-1726/14/4/013 10.1121/1.1466870 10.1016/j.compstruct.2012.06.003 10.1088/0964-1726/11/2/310 |
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