Estimating the unsteady angle of attack from blade pressure measurement on the NREL phase VI rotor in yaw using a free-wake vortex model

Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientificpeer-review

8 Citations (Scopus)
Original languageUndefined/Unknown
Title of host publicationProceedings of the 44th Aerospace sciences meeting and exhibit
Editors s.n.
Place of PublicationReno
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
Number of pages26
Publication statusPublished - 2006
Event44th Aerospace sciences meeting and exhibit - Reno
Duration: 9 Jan 200612 Jan 2006

Publication series

PublisherAmerican institute of aeronautics and astronautics


Conference44th Aerospace sciences meeting and exhibit


  • Conf.proc. > 3 pag

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