Preliminary assessment of the NACA0021 trailing edge wedge for wind turbine application
The airfoil blade is the primary component of a wind turbine, and its aerodynamic properties play a crucial role in determining the energy conversion efficiency of these blades. Many researchers have proposed different airfoil modifications intending to enhance the aerodynamic characteristics and li...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
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Elsevier
2023-11-01
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| Series: | Heliyon |
| Subjects: | |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2405844023084013 |
| _version_ | 1797429917726539776 |
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| author | Asmail A.M. Abdalkarem Roaa Ansaf Wan Khairul Muzammil Adnan Ibrahim Zambri Harun Ahmad Fazlizan |
| author_facet | Asmail A.M. Abdalkarem Roaa Ansaf Wan Khairul Muzammil Adnan Ibrahim Zambri Harun Ahmad Fazlizan |
| author_sort | Asmail A.M. Abdalkarem |
| collection | DOAJ |
| description | The airfoil blade is the primary component of a wind turbine, and its aerodynamic properties play a crucial role in determining the energy conversion efficiency of these blades. Many researchers have proposed different airfoil modifications intending to enhance the aerodynamic characteristics and limit the unsteady interaction with the atmospheric boundary layer. This study evaluates the benefits of mounting wedge tails (WTs) on the trailing edge of an airfoil. The aerodynamic characteristics of a 2-D, steady-state NACA 0021 airfoil featuring the wedge tails (WT) and fish wedge tails (FWT) were studied computationally by employing the shear stress transport (SST) k-ω turbulence model. Different WT and FWT configurations were studied at various wedge length (L) to wedge height (H) ratios, L/H, at the airfoil's trailing edge. The effects of different L/H ratios, including L/H > 1, L/H = 1, and L/H < 1, were considered in the present study to determine the optimal configuration to achieve the maximum glide ratio, CL/CD at the Reynolds number of 180,000. The findings indicate that the performance of the NACA 0021 airfoil was notably affected by the height of the tail; however, the length had only a minor impact when L/H was less than 1. The mounted FWT resulted in significant enhancements to both the lift and glide ratio of the airfoil. Specifically, the lift ratio experienced an increase of over 41 % compared to the clean airfoil, while the glide ratio increased by more than 31 %. These improvements were observed at an ideal height and length of 2.5 % and 1 % of the airfoil, respectively. Moreover, the mounted FWT performed better than the Gurney flap using the same configurations. |
| first_indexed | 2024-03-09T09:19:49Z |
| format | Article |
| id | doaj.art-8171ff05b90648b2892af0d50313ae8d |
| institution | Directory Open Access Journal |
| issn | 2405-8440 |
| language | English |
| last_indexed | 2024-03-09T09:19:49Z |
| publishDate | 2023-11-01 |
| publisher | Elsevier |
| record_format | Article |
| series | Heliyon |
| spelling | doaj.art-8171ff05b90648b2892af0d50313ae8d2023-12-02T07:01:25ZengElsevierHeliyon2405-84402023-11-01911e21193Preliminary assessment of the NACA0021 trailing edge wedge for wind turbine applicationAsmail A.M. Abdalkarem0Roaa Ansaf1Wan Khairul Muzammil2Adnan Ibrahim3Zambri Harun4Ahmad Fazlizan5Solar Energy Research Institute (SERI), University Kebangsaan Malaysia, 43600 Bangi, Selangor, MalaysiaDepartment of Mechanical and Manufacturing Engineering, Faculty of Engineering and Built Environment, University Kebangsaan Malaysia (UKM), Bangi, 43600, MalaysiaCentre of Research in Energy and Advanced Materials, Faculty of Engineering, University Malaysia Sabah, Jln. UMS, 88400, Kota Kinabalu, MalaysiaSolar Energy Research Institute (SERI), University Kebangsaan Malaysia, 43600 Bangi, Selangor, MalaysiaDepartment of Mechanical and Manufacturing Engineering, Faculty of Engineering and Built Environment, University Kebangsaan Malaysia (UKM), Bangi, 43600, MalaysiaSolar Energy Research Institute (SERI), University Kebangsaan Malaysia, 43600 Bangi, Selangor, Malaysia; Corresponding author.The airfoil blade is the primary component of a wind turbine, and its aerodynamic properties play a crucial role in determining the energy conversion efficiency of these blades. Many researchers have proposed different airfoil modifications intending to enhance the aerodynamic characteristics and limit the unsteady interaction with the atmospheric boundary layer. This study evaluates the benefits of mounting wedge tails (WTs) on the trailing edge of an airfoil. The aerodynamic characteristics of a 2-D, steady-state NACA 0021 airfoil featuring the wedge tails (WT) and fish wedge tails (FWT) were studied computationally by employing the shear stress transport (SST) k-ω turbulence model. Different WT and FWT configurations were studied at various wedge length (L) to wedge height (H) ratios, L/H, at the airfoil's trailing edge. The effects of different L/H ratios, including L/H > 1, L/H = 1, and L/H < 1, were considered in the present study to determine the optimal configuration to achieve the maximum glide ratio, CL/CD at the Reynolds number of 180,000. The findings indicate that the performance of the NACA 0021 airfoil was notably affected by the height of the tail; however, the length had only a minor impact when L/H was less than 1. The mounted FWT resulted in significant enhancements to both the lift and glide ratio of the airfoil. Specifically, the lift ratio experienced an increase of over 41 % compared to the clean airfoil, while the glide ratio increased by more than 31 %. These improvements were observed at an ideal height and length of 2.5 % and 1 % of the airfoil, respectively. Moreover, the mounted FWT performed better than the Gurney flap using the same configurations.http://www.sciencedirect.com/science/article/pii/S2405844023084013CFDPower augmentationAirfoilWedge flapWedge tail |
| spellingShingle | Asmail A.M. Abdalkarem Roaa Ansaf Wan Khairul Muzammil Adnan Ibrahim Zambri Harun Ahmad Fazlizan Preliminary assessment of the NACA0021 trailing edge wedge for wind turbine application Heliyon CFD Power augmentation Airfoil Wedge flap Wedge tail |
| title | Preliminary assessment of the NACA0021 trailing edge wedge for wind turbine application |
| title_full | Preliminary assessment of the NACA0021 trailing edge wedge for wind turbine application |
| title_fullStr | Preliminary assessment of the NACA0021 trailing edge wedge for wind turbine application |
| title_full_unstemmed | Preliminary assessment of the NACA0021 trailing edge wedge for wind turbine application |
| title_short | Preliminary assessment of the NACA0021 trailing edge wedge for wind turbine application |
| title_sort | preliminary assessment of the naca0021 trailing edge wedge for wind turbine application |
| topic | CFD Power augmentation Airfoil Wedge flap Wedge tail |
| url | http://www.sciencedirect.com/science/article/pii/S2405844023084013 |
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