Three dimensional separation effects on a simplified wind turbine blade
Abstract
A qualitative investigation of the three dimensional effects on a twisted non-rotating wing without tapering is performed, using a general purpose Navier-Stokes solver. Different location of twist center as well as different twist ratios are examined for fully attached flow. The case of a partially separated blade is investigated as well. The three dimensional effects are primarily identified by comparing the lift and C{sub p} distribution of the blade with the two dimensional counterpart.
- Authors:
-
- Risoe National Lab., Roskilde (Denmark)
- Technical Univ. of Denmark, Lyngby (Denmark). Dept. of Fluid Mechanics
- Publication Date:
- OSTI Identifier:
- 372131
- Report Number(s):
- CONF-960154-
ISBN 0-9648731-8-4; TRN: IM9641%%208
- Resource Type:
- Conference
- Resource Relation:
- Conference: Energy Week `96: American Society of Mechanical Engineers and American Petroleum Institute energy week conference and exhibition, Houston, TX (United States), 21 Jan - 2 Feb 1996; Other Information: PBD: 1996; Related Information: Is Part Of Energy week `96: Conference papers. Book 8: Wind energy; PB: 218 p.
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 17 WIND ENERGY; WIND TURBINES; AERODYNAMICS; CONTROL THEORY; TURBINE BLADES; TURBULENT FLOW
Citation Formats
Soerensen, N N, and Michelsen, J A. Three dimensional separation effects on a simplified wind turbine blade. United States: N. p., 1996.
Web.
Soerensen, N N, & Michelsen, J A. Three dimensional separation effects on a simplified wind turbine blade. United States.
Soerensen, N N, and Michelsen, J A. 1996.
"Three dimensional separation effects on a simplified wind turbine blade". United States.
@article{osti_372131,
title = {Three dimensional separation effects on a simplified wind turbine blade},
author = {Soerensen, N N and Michelsen, J A},
abstractNote = {A qualitative investigation of the three dimensional effects on a twisted non-rotating wing without tapering is performed, using a general purpose Navier-Stokes solver. Different location of twist center as well as different twist ratios are examined for fully attached flow. The case of a partially separated blade is investigated as well. The three dimensional effects are primarily identified by comparing the lift and C{sub p} distribution of the blade with the two dimensional counterpart.},
doi = {},
url = {https://www.osti.gov/biblio/372131},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Oct 01 00:00:00 EDT 1996},
month = {Tue Oct 01 00:00:00 EDT 1996}
}
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