Preliminary Study on a Wide-Speed-Range Helicopter Rotor/Turboshaft System
Author:
Affiliation:
1. University of Padua, 35131 Padua, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031526
Reference15 articles.
1. "PW207D Engine," Pratt & Whitney Canada, Longueuil, Quebec, Canada, http://www.pwc.ca/en/engines/pw207d [retrieved June 2012].
2. Benefits of variable rotor speed in integrated helicopter/engine control
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