A smart rotor configuration with linear quadratic control of adaptive trailing edge flaps for active load alleviation
Author:
Affiliation:
1. Department of Wind Energy; Technical University of Denmark; Denmark
2. Department of Informatics and Mathematical Modeling; Technical University of Denmark; Denmark
Funder
H�jteknologifonden, Advanced Technology Projects 2007
Publisher
Wiley
Subject
Renewable Energy, Sustainability and the Environment
Reference41 articles.
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4. Computational study of the Riso-B1-18 airfoil with a hinged flap providing variable trailing edge geometry;Troldborg;Wind Engineering,2005
5. Potential load reduction using airfoils with variable trailing edge geometry;Buhl;Transactions of the ASME.Journal of Solar Energy Engineering,2005
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