Analysis of the rub-impact forces between a controlled nonlinear rotating shaft system and the electromagnet pole legs
From MaRDI portal
Publication:823505
DOI10.1016/j.apm.2021.01.008zbMath1481.70060OpenAlexW3118456973MaRDI QIDQ823505
Emad Abouel Nasr, Mohammed A. EL-meligy, Emad Mahrous Awwad, Nasser A. Saeed
Publication date: 24 September 2021
Published in: Applied Mathematical Modelling (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.apm.2021.01.008
Poincaré mapfrequency spectrumasymmetric rotating shaftfull annular rubquasiperiodic partial rubrub-impact forces
Cites Work
- Nonlinear vibration phenomenon of an aircraft rub-impact rotor system due to hovering flight
- The effect of transverse crack upon parametric instability of a rotor-bearing system with an asymmetric disk
- Dynamic characteristics analysis of a rotor-stator system under different rubbing forms
- Passive vibration absorbers for vibration reduction in the multi-bladed rotor with rotor and stator contact
- Vibration mitigation of a flexible bladed rotor dynamic system with passive dynamic absorbers
- Sensitivity analysis and vibration control of asymmetric nonlinear rotating shaft system utilizing 4-pole AMBs as an actuator
- Time-delayed control to suppress the nonlinear vibrations of a horizontally suspended Jeffcott-rotor system
- On the steady-state forward and backward whirling motion of asymmetric nonlinear rotor system
- Vibration of asymmetric rotor supported by oil film bearings
- Vibration Suppression of Nonlinear Rotor Systems Using a Dynamic Damper
This page was built for publication: Analysis of the rub-impact forces between a controlled nonlinear rotating shaft system and the electromagnet pole legs
