Aerodynamic Characteristics of Shark Scale-Based Vortex Generators upon Symmetrical Airfoil
A series of wind tunnel tests were carried out to determine the effect of shark scale-based vortex generators (SSVG) on a NACA 0015 symmetrical airfoil’s aerodynamic characteristics. Three different sets of SSVG with varying geometrical parameters, such as chord length, amplitude, and wavelength, we...
| Main Authors: | , , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2021-03-01
|
| Series: | Energies |
| Subjects: | |
| Online Access: | https://www.mdpi.com/1996-1073/14/7/1808 |
| _version_ | 1797540149487206400 |
|---|---|
| author | S. Arunvinthan V.S. Raatan S. Nadaraja Pillai Amjad A. Pasha M. M. Rahman Khalid A. Juhany |
| author_facet | S. Arunvinthan V.S. Raatan S. Nadaraja Pillai Amjad A. Pasha M. M. Rahman Khalid A. Juhany |
| author_sort | S. Arunvinthan |
| collection | DOAJ |
| description | A series of wind tunnel tests were carried out to determine the effect of shark scale-based vortex generators (SSVG) on a NACA 0015 symmetrical airfoil’s aerodynamic characteristics. Three different sets of SSVG with varying geometrical parameters, such as chord length, amplitude, and wavelength, were designed and fabricated using 3D printing. The SSVG models were blended to the baseline NACA 0015 symmetrical airfoil. The wind tunnel experiments were performed over the test airfoil mounted with different sets of SSVG at various angles of attack, ranging from 0° to 24° in increments of 3°, and operating in the range of Re = 2 × 10<sup>5</sup>. The results revealed that the SSVG blended test airfoil reduced the drag and increased the maximum coefficient of lift (C<sub>Lmax</sub>), thereby enhancing the overall aerodynamic performance. The SSVG offered noteworthy aerodynamic benefits by effectively altering the flow and causing significant spanwise variation in the flow properties. Additionally, attempts were made to identify the optimum chordwise location to blend the SSVG for effective use. |
| first_indexed | 2024-03-10T12:55:56Z |
| format | Article |
| id | doaj.art-3ee97cba8dfb44b3bc73ce7ee2b17755 |
| institution | Directory Open Access Journal |
| issn | 1996-1073 |
| language | English |
| last_indexed | 2024-03-10T12:55:56Z |
| publishDate | 2021-03-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Energies |
| spelling | doaj.art-3ee97cba8dfb44b3bc73ce7ee2b177552023-11-21T11:52:30ZengMDPI AGEnergies1996-10732021-03-01147180810.3390/en14071808Aerodynamic Characteristics of Shark Scale-Based Vortex Generators upon Symmetrical AirfoilS. Arunvinthan0V.S. Raatan1S. Nadaraja Pillai2Amjad A. Pasha3M. M. Rahman4Khalid A. Juhany5Turbulence and Flow Control Lab, School of Mechanical Engineering, SASTRA Deemed University, Thanjavur, Tamil Nadu 613401, IndiaTurbulence and Flow Control Lab, School of Mechanical Engineering, SASTRA Deemed University, Thanjavur, Tamil Nadu 613401, IndiaTurbulence and Flow Control Lab, School of Mechanical Engineering, SASTRA Deemed University, Thanjavur, Tamil Nadu 613401, IndiaDepartment of Aerospace Engineering, King Abdulaziz University, Jeddah 21589, Saudi ArabiaPhysical Science and Engineering Division, King Abdullah University of Science & Technology, Thuwal 23955, Saudi ArabiaDepartment of Aerospace Engineering, King Abdulaziz University, Jeddah 21589, Saudi ArabiaA series of wind tunnel tests were carried out to determine the effect of shark scale-based vortex generators (SSVG) on a NACA 0015 symmetrical airfoil’s aerodynamic characteristics. Three different sets of SSVG with varying geometrical parameters, such as chord length, amplitude, and wavelength, were designed and fabricated using 3D printing. The SSVG models were blended to the baseline NACA 0015 symmetrical airfoil. The wind tunnel experiments were performed over the test airfoil mounted with different sets of SSVG at various angles of attack, ranging from 0° to 24° in increments of 3°, and operating in the range of Re = 2 × 10<sup>5</sup>. The results revealed that the SSVG blended test airfoil reduced the drag and increased the maximum coefficient of lift (C<sub>Lmax</sub>), thereby enhancing the overall aerodynamic performance. The SSVG offered noteworthy aerodynamic benefits by effectively altering the flow and causing significant spanwise variation in the flow properties. Additionally, attempts were made to identify the optimum chordwise location to blend the SSVG for effective use.https://www.mdpi.com/1996-1073/14/7/1808aerodynamic efficiencyairfoilsforce balanceshark scalevortex generatorswind tunnel |
| spellingShingle | S. Arunvinthan V.S. Raatan S. Nadaraja Pillai Amjad A. Pasha M. M. Rahman Khalid A. Juhany Aerodynamic Characteristics of Shark Scale-Based Vortex Generators upon Symmetrical Airfoil Energies aerodynamic efficiency airfoils force balance shark scale vortex generators wind tunnel |
| title | Aerodynamic Characteristics of Shark Scale-Based Vortex Generators upon Symmetrical Airfoil |
| title_full | Aerodynamic Characteristics of Shark Scale-Based Vortex Generators upon Symmetrical Airfoil |
| title_fullStr | Aerodynamic Characteristics of Shark Scale-Based Vortex Generators upon Symmetrical Airfoil |
| title_full_unstemmed | Aerodynamic Characteristics of Shark Scale-Based Vortex Generators upon Symmetrical Airfoil |
| title_short | Aerodynamic Characteristics of Shark Scale-Based Vortex Generators upon Symmetrical Airfoil |
| title_sort | aerodynamic characteristics of shark scale based vortex generators upon symmetrical airfoil |
| topic | aerodynamic efficiency airfoils force balance shark scale vortex generators wind tunnel |
| url | https://www.mdpi.com/1996-1073/14/7/1808 |
| work_keys_str_mv | AT sarunvinthan aerodynamiccharacteristicsofsharkscalebasedvortexgeneratorsuponsymmetricalairfoil AT vsraatan aerodynamiccharacteristicsofsharkscalebasedvortexgeneratorsuponsymmetricalairfoil AT snadarajapillai aerodynamiccharacteristicsofsharkscalebasedvortexgeneratorsuponsymmetricalairfoil AT amjadapasha aerodynamiccharacteristicsofsharkscalebasedvortexgeneratorsuponsymmetricalairfoil AT mmrahman aerodynamiccharacteristicsofsharkscalebasedvortexgeneratorsuponsymmetricalairfoil AT khalidajuhany aerodynamiccharacteristicsofsharkscalebasedvortexgeneratorsuponsymmetricalairfoil |