Abstract
The experimental feasibility of a vibration based approach to identify damage in an advanced composite aircraft structure is presented. Analysis showed that the Modal Strain Energy Damage Index (MSE-DI) algorithm can be used to detect and localize single and multiple damage scenarios by using modal data. However, this method is less suitable to quantify the severity in terms of mechanical properties. Based on the concept of dimensional reduction it is suggested to move to a higher dimensional subset of parameters. A combination of damage sensitive features is required to enclose all levels of damage identification.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of the 8th International Workshop on Structural Health Monitoring 2011 |
| Editors | F.K. Chang, A. Guemes |
| Place of Publication | Lancaster, Pennsylvania, U.S.A. |
| Publisher | DEStech Publications, Inc |
| Pages | 1053-1061 |
| Publication status | Published - 2011 |
| Event | 8th International Workshop on Structural Health Monitoring, IWSHM 2011 - Stanford University, Stanford, United States Duration: 13 Sept 2011 → 15 Sept 2011 Conference number: 8 |
Publication series
| Name | |
|---|---|
| Publisher | DEStech Publications, Inc. |
Workshop
| Workshop | 8th International Workshop on Structural Health Monitoring, IWSHM 2011 |
|---|---|
| Abbreviated title | IWSHM |
| Country/Territory | United States |
| City | Stanford |
| Period | 13/09/11 → 15/09/11 |
Keywords
- METIS-282562
- IR-79160
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