Improvement of Noise Reduction and Performance for a Helicopter Model Rotor Blade by Active Twist Actuation
35th, European rotorcraft forum ; 2009 ; Hamburg, Germany
01.01.2009
1157 pages
Held on CD-ROM; Held in e-store (RMS)
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Helicopter performance improvement by variable rotor speed and variable blade twist
Online Contents | 2016
|Helicopter flight performance improvement by dynamic blade twist
Online Contents | 2016
|Numerical optimization of helicopter rotor blade design for active twist control
DOAJ | 2007
|