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

6 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)
Pages1-26
Number of pages26
Publication statusPublished - 2006
Event44th Aerospace sciences meeting and exhibit - Reno
Duration: 9 Jan 200612 Jan 2006

Publication series

Name
PublisherAmerican institute of aeronautics and astronautics

Conference

Conference44th Aerospace sciences meeting and exhibit
Period9/01/0612/01/06

Keywords

  • Conf.proc. > 3 pag

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