## A method is presentedfor the stability analysis of systems which include a number of delay elements. The method is based on the transmission line modelling method in which all dynamic elements are modelled by ideal, lossless transmission lines. The resulting system can be mathematically represent
Vibration analysis of distributed-lumped rotor systems
β Scribed by M. Aleyaasin; M. Ebrahimi; R. Whalley
- Publisher
- Elsevier Science
- Year
- 2000
- Tongue
- English
- Weight
- 244 KB
- Volume
- 189
- Category
- Article
- ISSN
- 0045-7825
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β¦ Synopsis
In this paper a distributed-lumped model for the analysis of the Β―exural vibrations of a rotor-bearing system is considered. A general formula for the determinant of the tri-diagonal partitioned matrix description of the system is derived. This enables the irrational characteristic determinant of the system model to be obtained by the dynamic stiness matrix method. The results obtained are compared to those acquired from the transfer matrix method. The error source in the computation of the natural frequencies by the dynamic stiness matrix method is discussed. It is shown that by implementing the transfer matrix method the natural frequencies obtained are of greater accuracy. A numerical example illustrating the two methods, is presented and the results achieved are commented upon.
π SIMILAR VOLUMES
Exact solutions for a distributed parameter system are of great use for the physical understanding of the system or the sensitivity analysis and design of the system. However, exact or closed-form solutions for multi-stepped rotor-bearing systems with distributed parameters have been rarely investig
A dynamic model is derived for misaligned rotor-ball bearing systems driven through a flexible coupling by treating the reaction loads and deformations at the bearing and coupling elements as the misalignment effect. In order to verify the validity of the misaligned rotor system model, experiments a
The Lyapunov-function method is used to investigate the stability of systems with distributed parameters and lumped forces described by linear partial differential equations (for example, elastic structures with lumped masses, dampers, elastic aircraft with rigid control rudders, etc.). By introduci