Abstract
The motivation of this paper is to achieve a rapid condition assessment and identification for aero-space structures. For such a circumstance, transmissibility is a good vibration-domain feature for damage detection and localization, highlighting the sensitivity of the relative dynamics between any two interest points on the structure to many forms of damage (such as connection losses). With a quantified uncertainty model of transmissibility available, test results may be compared to baseline (undamaged) statistics, and statistical significance under certain confidence level may be found. Receiver operating characteristic curves suggest the optimized threshold of detection that balances detections and false alarms. In this paper, three such models are presented, and the aforementioned statistical identifications are validated through a plate structure with a single-edge clamped boundary condition. The benchmark test results show very good consistency with the model prediction and the robustness to different noise contamination situations.
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Acknowledgments
This material is based on research sponsored by the Army Research Laboratory and managed by the Air Force Research Laboratory, Space Vehicles Directorate, under agreement number FA9453-09-1-0315 P00001. The U.S. Government is authorized to reproduce and distribute reprints for Governmental purposes notwithstanding any copyright notation thereon. The views and conclusions contained herein are those of the authors and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of Army Research Laboratory, Air Force Research Laboratory, or the U.S. Government.
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© 2012 The Society for Experimental Mechanics, Inc. 2012
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Mao, Z., Todd, M. (2012). Rapid Structural Condition Assessment Using Transmissibility with Quantified Confidence for Decision Making. In: Simmermacher, T., Cogan, S., Horta, L., Barthorpe, R. (eds) Topics in Model Validation and Uncertainty Quantification, Volume 4. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, New York, NY. https://doi.org/10.1007/978-1-4614-2431-4_14
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DOI: https://doi.org/10.1007/978-1-4614-2431-4_14
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