Abstract
Vibration testing is used as a means of validating Finite Element models and also to measure modal damping. The classical approach typically assumes that the system is linear. With the need to improve system performance, aerospace and automotive structures are being designed with much lighter construction and also much less inherent damping, consequently structural nonlinearities have a much greater effect on performance. Although there has been significant effort towards the development of nonlinear modal analysis methodologies, these techniques are still not at a stage where they can be used on industrial size structures. This paper describes an experimental investigation on a structure with the characteristics of large scale weakly nonlinear industrial structure. It presents a procedure able to extract backbone curves from decay responses. This enables measurements to be made in regimes where nonlinear effects are more significant. Conclusions are drawn as to the most effective approaches for future developments and industrial application.
Original language | English |
---|---|
Title of host publication | Proceedings of ISMA 2014 - International Conference on Noise and Vibration Engineering and USD 2014 - International Conference on Uncertainty in Structural Dynamics |
Publisher | Katholieke Universiteit Leuven |
Pages | 1199-1210 |
Number of pages | 12 |
ISBN (Print) | 9789073802919 |
Publication status | Published - 2014 |
Event | 26th International Conference on Noise and Vibration Engineering, ISMA 2014, Including the 5th International Conference on Uncertainty in Structural Dynamics, USD 2014 - Leuven, Belgium Duration: 15 Sept 2014 → 17 Sept 2014 |
Conference
Conference | 26th International Conference on Noise and Vibration Engineering, ISMA 2014, Including the 5th International Conference on Uncertainty in Structural Dynamics, USD 2014 |
---|---|
Country/Territory | Belgium |
City | Leuven |
Period | 15/09/14 → 17/09/14 |