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  4. Assessment of weak compressibility in actuator line simulations of wind turbine wakes
 
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Assessment of weak compressibility in actuator line simulations of wind turbine wakes

Citation Link: https://doi.org/10.15480/882.3018
Publikationstyp
Journal Article
Date Issued
2020-09-21
Sprache
English
Author(s)
Asmuth, Henrik  
Janßen, Christian Friedrich  orcid-logo
Olivares-Espinosa, Hugo  
Nilsson, Karl  
Ivanell, Stefan  
Institut
Fluiddynamik und Schiffstheorie M-8  
TORE-DOI
10.15480/882.3018
TORE-URI
http://hdl.handle.net/11420/7704
Journal
Journal of physics. Conference Series  
Volume
1618
Issue
6
Article Number
062057
Citation
Journal of Physics: Conference Series 6 (1618): 062057 (2020)
Publisher DOI
10.1088/1742-6596/1618/6/062057
Scopus ID
2-s2.0-85092457297
Publisher
IOP Publ.
The trend of increasing rotor diameters and tip-speeds has brought about concerns of non-negligible compressibility effects in wind turbine aerodynamics. The investigation of such effects on wakes is particularly difficult when using actuator line models (ALM). This is because crucial regions of the flow, i.e. the direct vicinity of the blade, are not simulated but represented by body forces. To separately assess the impact of compressibility on the wake and the ALM itself, we conduct large-eddy simulations (LES) where the forces of the ALM are prescribed and based on the local sampled velocity (standard procedure), respectively. The LES are based on the weakly-compressible Lattice Boltzmann Method (LBM). Further to the comparison of (near-)incompressible to compressible simulations we investigate cases with artificially increased compressibility. This is commonly done in weakly-compressible approaches to reduce the computational demand. The investigation with prescribed forces shows that compressibility effects in the wake flow are negligible. Small differences in the wake velocity (of max. 1%) are found to be related to local compressibility effects in the direct vicinity of the ALM. Most significantly, compressibility is found to affect the sampled velocity and thereby accuracy of the ALM.
DDC Class
620: Ingenieurwissenschaften
Publication version
publishedVersion
Lizenz
https://creativecommons.org/licenses/by/3.0/
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