Large-eddy simulations for wind turbine blade: dynamic stall and rotational augmentation
Large-eddy simulations for wind turbine blade: dynamic stall and rotational augmentation
Wind turbines operate in the atmospheric boundary layer and their rotating mechanisms provide complicated aerodynamic phenomena within their operating environments. When the upstream wind is uniform and normal to the plane of a rotating blade, rotational effects (i.e. rotational augmentation) emerge. Rotational augmentation means that stall occurs at a higher angle of attack on the rotating blade section than it does on an analogous stationary airfoil.
978-3-319-14447-4
369-375
Kim, Yusik
5898caed-b9e9-4c9c-84cb-5634b0eec174
Castro, I.P.
66e6330d-d93a-439a-a69b-e061e660de61
Xie, Z.T.
98ced75d-5617-4c2d-b20f-7038c54f4ff0
28 January 2015
Kim, Yusik
5898caed-b9e9-4c9c-84cb-5634b0eec174
Castro, I.P.
66e6330d-d93a-439a-a69b-e061e660de61
Xie, Z.T.
98ced75d-5617-4c2d-b20f-7038c54f4ff0
Kim, Yusik, Castro, I.P. and Xie, Z.T.
(2015)
Large-eddy simulations for wind turbine blade: dynamic stall and rotational augmentation.
In,
Fröhlich, Jochen, Kuerten, Hans, Guerts, Bernard J. and Amenio, Vincenzo
(eds.)
Direct and Large-Eddy Simulation IX.
(Direct and Large Eddy Simulation, 20)
Berlin, DE.
Springer, .
(doi:10.1007/978-3-319-14448-1_46).
Record type:
Book Section
Abstract
Wind turbines operate in the atmospheric boundary layer and their rotating mechanisms provide complicated aerodynamic phenomena within their operating environments. When the upstream wind is uniform and normal to the plane of a rotating blade, rotational effects (i.e. rotational augmentation) emerge. Rotational augmentation means that stall occurs at a higher angle of attack on the rotating blade section than it does on an analogous stationary airfoil.
Text
__soton.ac.uk_ude_PersonalFiles_Users_zxie_mydocuments_Original_ref_paper_xiezt_DLES_DLES2012.pdf
- Accepted Manuscript
More information
e-pub ahead of print date: 28 January 2015
Published date: 28 January 2015
Organisations:
Aerodynamics & Flight Mechanics Group
Identifiers
Local EPrints ID: 378294
URI: http://eprints.soton.ac.uk/id/eprint/378294
ISBN: 978-3-319-14447-4
ISSN: 1382-4309
PURE UUID: 05c74412-cdec-4b2a-8ba2-05564a2d3a4c
Catalogue record
Date deposited: 01 Jul 2015 11:03
Last modified: 15 Mar 2024 03:20
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Contributors
Author:
Yusik Kim
Editor:
Jochen Fröhlich
Editor:
Hans Kuerten
Editor:
Bernard J. Guerts
Editor:
Vincenzo Amenio
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