Performance of twist-coupled blades on variable speed rotors
Author:
Affiliation:
1. Sandia National Labs., Albuquerque, NM
2. Windward Engineering, Salt Lake City, UT
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-62
Reference10 articles.
1. Aeroelastic behavior of twist-coupled HAWT blades
2. Load mitigation with twist-coupled HAWT blades
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