Turning maneuver caused response in an aircraft rotor-ball bearing system
Authors:
- 9 October 2014
- journal article
- Published by Springer Nature in Nonlinear Dynamics
- Vol. 79 (1) , 229-240
Abstract
No abstract availableKeywords
This publication has 33 references indexed in Scilit:
- Nonlinear vibration phenomenon of an aircraft rub-impact rotor system due to hovering flightCommunications in Nonlinear Science and Numerical Simulation, 2014
- Analysis of the nonlinear dynamic response of a rotor supported on ball bearings with floating-ring squeeze film dampersMechanism and Machine Theory, 2013
- Non-linear dynamics and contacts of an unbalanced flexible rotor supported on ball bearingsMechanism and Machine Theory, 2009
- Experiments on routes to chaos in ball bearingsJournal of Sound and Vibration, 2008
- Effect of rotational speed fluctuations on the dynamic behaviour of rolling element bearings with radial clearancesInternational Journal of Mechanical Sciences, 2006
- Stability analysis of a rotor bearing system due to surface waviness and number of ballsInternational Journal of Mechanical Sciences, 2004
- The effect of speed of balanced rotor on nonlinear vibrations associated with ball bearingsInternational Journal of Mechanical Sciences, 2003
- EFFECT OF RADIAL INTERNAL CLEARANCE OF A BALL BEARING ON THE DYNAMICS OF A BALANCED HORIZONTAL ROTORJournal of Sound and Vibration, 2000
- DYNAMIC RESPONSE OF AN UNBALANCED ROTOR SUPPORTED ON BALL BEARINGSJournal of Sound and Vibration, 2000
- Modelling and Vibration Analysis of Misaligned Rotor-Ball Bearing SystemsJournal of Sound and Vibration, 1999