Vibrations in helicopters ‐ reduction and monitoring
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 April 1997
Abstract
Describes the Westland active control of structural response (ACSR) technique for reducing and alleviating vibration. Examines a refined coupled rotor/flexible fuselage model based on the ACSR approach. Reports on vibration health monitoring (VHM) which has been developed by Westland and details further work which is continuing in this field.
Keywords
Citation
Ford, T. (1997), "Vibrations in helicopters ‐ reduction and monitoring", Aircraft Engineering and Aerospace Technology, Vol. 69 No. 2, pp. 119-125. https://doi.org/10.1108/00022669710164448
Publisher
:MCB UP Ltd
Copyright © 1997, MCB UP Limited