Abstract
In this paper, we present the results of an investigation of significant damping effects and the ability to locate damage. A three-bay, vertically cantilevered laboratory truss testbed was developed to exhibit beam-like response for the first three modes (a pair of first bending modes in orthogonal directions and a torsional mode). Truss members were removed from the testbed to simulate various damage scenarios with reduced stiffness. In addition, up to four visco-elastic damping struts were placed in the truss testbed in various configurations to affect the damping of certain modes of the structure. A comprehensive test matrix of damping and damage effects was designed and completed to construct the data base for the damping and damage identification evaluations. Two representative visco-elastic struts were also tested individually to determine their stiffness and damping characteristics. The damage detection process used the differences between pre- and post-damage vibration characteristics, along with a structural model, to successfully locate and quantify the extent of structural damage in all cases. Damping matrix models were also identified and evaluated.
Original language | English |
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Title of host publication | 16th Biennial Conference on Mechanical Vibration and Noise |
ISBN (Electronic) | 9780791880432 |
DOIs | |
State | Published - 1997 |
Event | ASME 1997 Design Engineering Technical Conferences, DETC 1997 - Sacramento, United States Duration: Sep 14 1997 → Sep 17 1997 |
Publication series
Name | Proceedings of the ASME Design Engineering Technical Conference |
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Volume | 1D-1997 |
Conference
Conference | ASME 1997 Design Engineering Technical Conferences, DETC 1997 |
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Country/Territory | United States |
City | Sacramento |
Period | 9/14/97 → 9/17/97 |
Bibliographical note
Publisher Copyright:© 1997 American Society of Mechanical Engineers (ASME). All rights reserved.
Funding
The first two authors efforts were partially supported by McDonnell Douglas Aerospace, Houston, TX. The authors would like to thank Alex Chapman, a University of Kentucky undergraduate student, for his work in testing the truss and performing the modal identification. The authors also acknowledge the work of Raul Blanco, a University of Houston Masters student, who performed the individual strut tests and analysis.
Funders | Funder number |
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University of Kentucky | |
McDonnell Douglas Aerospace |
ASJC Scopus subject areas
- Mechanical Engineering
- Computer Graphics and Computer-Aided Design
- Computer Science Applications
- Modeling and Simulation