Vibration based structural health monitoring of a composite plate with stiffeners

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

4 Citations (Scopus)
9 Downloads (Pure)

Abstract

A vibration based damage identification algorithm is implemented to assess the damage of a thin-walled composite structure. The structure analysed is a skin with stiffeners, as frequently applied in aircraft components. Both experimental and numerical studies on a single composite skin--stiffener structure showed that the modal strain energy damage index (MSE--DI) algorithm is a suitable method for the detection and localization of a delamination of the stiffener from the skin. A recent study on a strip with a single stiffener and an artificial delamination is extended to a study on a plate with two stiffeners and an impact induced delamination damage.
Original languageUndefined
Title of host publicationProceedings of the ISMA conference
EditorsP Sas
Place of PublicationLeuven
PublisherKatholieke Universiteit Leuven
Pages909-924
Publication statusPublished - 22 Sep 2010
Event24th International Conference on Noise and Vibration Engineering, ISMA 2010 - Leuven, Belgium
Duration: 20 Sep 201022 Sep 2010
Conference number: 24
http://past.isma-isaac.be/isma2010/

Publication series

Name
PublisherKU Leuven

Conference

Conference24th International Conference on Noise and Vibration Engineering, ISMA 2010
Abbreviated titleISMA
CountryBelgium
CityLeuven
Period20/09/1022/09/10
Internet address

Keywords

  • METIS-266989
  • IR-73137

Cite this

Loendersloot, R., Ooijevaar, T. H., Warnet, L., de Boer, A., & Akkerman, R. (2010). Vibration based structural health monitoring of a composite plate with stiffeners. In P. Sas (Ed.), Proceedings of the ISMA conference (pp. 909-924). Leuven: Katholieke Universiteit Leuven.
Loendersloot, Richard ; Ooijevaar, T.H. ; Warnet, Laurent ; de Boer, Andries ; Akkerman, Remko. / Vibration based structural health monitoring of a composite plate with stiffeners. Proceedings of the ISMA conference. editor / P Sas. Leuven : Katholieke Universiteit Leuven, 2010. pp. 909-924
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title = "Vibration based structural health monitoring of a composite plate with stiffeners",
abstract = "A vibration based damage identification algorithm is implemented to assess the damage of a thin-walled composite structure. The structure analysed is a skin with stiffeners, as frequently applied in aircraft components. Both experimental and numerical studies on a single composite skin--stiffener structure showed that the modal strain energy damage index (MSE--DI) algorithm is a suitable method for the detection and localization of a delamination of the stiffener from the skin. A recent study on a strip with a single stiffener and an artificial delamination is extended to a study on a plate with two stiffeners and an impact induced delamination damage.",
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publisher = "Katholieke Universiteit Leuven",
pages = "909--924",
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Loendersloot, R, Ooijevaar, TH, Warnet, L, de Boer, A & Akkerman, R 2010, Vibration based structural health monitoring of a composite plate with stiffeners. in P Sas (ed.), Proceedings of the ISMA conference. Katholieke Universiteit Leuven, Leuven, pp. 909-924, 24th International Conference on Noise and Vibration Engineering, ISMA 2010, Leuven, Belgium, 20/09/10.

Vibration based structural health monitoring of a composite plate with stiffeners. / Loendersloot, Richard; Ooijevaar, T.H.; Warnet, Laurent; de Boer, Andries; Akkerman, Remko.

Proceedings of the ISMA conference. ed. / P Sas. Leuven : Katholieke Universiteit Leuven, 2010. p. 909-924.

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

TY - GEN

T1 - Vibration based structural health monitoring of a composite plate with stiffeners

AU - Loendersloot, Richard

AU - Ooijevaar, T.H.

AU - Warnet, Laurent

AU - de Boer, Andries

AU - Akkerman, Remko

PY - 2010/9/22

Y1 - 2010/9/22

N2 - A vibration based damage identification algorithm is implemented to assess the damage of a thin-walled composite structure. The structure analysed is a skin with stiffeners, as frequently applied in aircraft components. Both experimental and numerical studies on a single composite skin--stiffener structure showed that the modal strain energy damage index (MSE--DI) algorithm is a suitable method for the detection and localization of a delamination of the stiffener from the skin. A recent study on a strip with a single stiffener and an artificial delamination is extended to a study on a plate with two stiffeners and an impact induced delamination damage.

AB - A vibration based damage identification algorithm is implemented to assess the damage of a thin-walled composite structure. The structure analysed is a skin with stiffeners, as frequently applied in aircraft components. Both experimental and numerical studies on a single composite skin--stiffener structure showed that the modal strain energy damage index (MSE--DI) algorithm is a suitable method for the detection and localization of a delamination of the stiffener from the skin. A recent study on a strip with a single stiffener and an artificial delamination is extended to a study on a plate with two stiffeners and an impact induced delamination damage.

KW - METIS-266989

KW - IR-73137

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EP - 924

BT - Proceedings of the ISMA conference

A2 - Sas, P

PB - Katholieke Universiteit Leuven

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Loendersloot R, Ooijevaar TH, Warnet L, de Boer A, Akkerman R. Vibration based structural health monitoring of a composite plate with stiffeners. In Sas P, editor, Proceedings of the ISMA conference. Leuven: Katholieke Universiteit Leuven. 2010. p. 909-924