A Parametric Study of On-Blade Control Device Performance for Helicopter Vibration and Noise Reduction
International annual forum; 70th, American Helicopter Society ; 2014 ; Montreal, Canada
01.01.2014
15 pages
Includes bibliographical references and author index.
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Reduction of Helicopter BVI Noise, Vibration, and Power Consumption Through Individual Blade Control
British Library Conference Proceedings | 1995
|Helicopter Vibration Reduction and Damping Enhancement Using Individual Blade Control
Online Contents | 2004
|Helicopter vibration reduction in forward flight using blade integral twist control
Tema Archiv | 2002
|