2015
DOI: 10.1016/j.enconman.2015.09.053
|View full text |Cite
|
Sign up to set email alerts
|

On the influence of virtual camber effect on airfoil polars for use in simulations of Darrieus wind turbines

Abstract: Darrieus vertical-axis wind turbines are experiencing renewed interest from researchers and manufacturers, though their efficiencies still lag those of horizontal-axis wind turbines. A better understanding of their aerodynamics is required to improve on designs, for example through the development of more accurate low-order (e.g. blade element momentum) models. Many of these models neglect the impact of the curved paths that are followed by blades on their performance. It has been theorized that the curved str… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
25
0

Year Published

2017
2017
2023
2023

Publication Types

Select...
6
3

Relationship

1
8

Authors

Journals

citations
Cited by 88 publications
(29 citation statements)
references
References 31 publications
0
25
0
Order By: Relevance
“…Migliore et al 71 illustrated that the flow curvature effects became more pronounced at large ratio. The blade performance will be modified due to the curvature effects and it must be considered when translating conventional aerofoil data for VAWT applications, as confirmed by a study performed by Rainbird et al 72 . Figure 7 Schematic drawing of curvature effects for symmetric blades moving in a curvilinear flow 71 Due to the orientation of the virtual camber, an additional normal force acts toward the centre of rotation and the normal force is increased during the upstream pass and decreased during the downstream pass.…”
Section: Curvaturementioning
confidence: 86%
“…Migliore et al 71 illustrated that the flow curvature effects became more pronounced at large ratio. The blade performance will be modified due to the curvature effects and it must be considered when translating conventional aerofoil data for VAWT applications, as confirmed by a study performed by Rainbird et al 72 . Figure 7 Schematic drawing of curvature effects for symmetric blades moving in a curvilinear flow 71 Due to the orientation of the virtual camber, an additional normal force acts toward the centre of rotation and the normal force is increased during the upstream pass and decreased during the downstream pass.…”
Section: Curvaturementioning
confidence: 86%
“…The most popular choice of airfoils for Darrieus turbines are symmetrical NACA profiles such as NACA 0015, 0018, and 0021, as they are experimentally validated for the range of Re that a VAWT typically experiences while in operation. Though it seems logical and efficient to use symmetrical airfoils as the suction and pressure side are reversed during the upwind and downwind rotation, the cambered airfoils are preferred from the self-starting perspective, especially for the fixed pitch VAWT as evaluated by Rainbird [28]. The airfoils should generate sufficient lift at low Re of 10 3 to 10 4 to overcome the resistive and inertial torque of the turbine to self-start.…”
Section: Camber and Symmetric Airfoilsmentioning
confidence: 99%
“…Symmetrical NACA 0015 airfoil with a 15% thickness to chord ratio has been chosen for this study. It is an indisputable fact that a cambered airfoil is preferable for the VAWT, due to the curved nature of the airfoil as reported by [39][40][41]. However, VAWT researchers have used one of the original NACA four digit series airfoil sections, usually either a NACA 0012 or a NACA 0015 section.…”
Section: Selection Of Airfoilmentioning
confidence: 99%