Aerodynamic Characteristics Improving of S809 Airfoil in Wind Turbine with Microtab
In present work numerical two dimensions, steady, incompressible, turbulent flow past S809 wind turbine airfoil with microtab at 95% of chord length of leading edge in lower surface is analyzed by Fluent (6.2) program for model consists of S809 airfoil without and with microtab at 95% of chord line...
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| Format: | Article |
| Language: | English |
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Unviversity of Technology- Iraq
2012-10-01
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| Series: | Engineering and Technology Journal |
| Subjects: | |
| Online Access: | https://etj.uotechnology.edu.iq/article_66155_0313bee27887938f4d5d68eb2d2a0fa0.pdf |
| _version_ | 1797325492694548480 |
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| author | Ressan Faris Al-Maliky |
| author_facet | Ressan Faris Al-Maliky |
| author_sort | Ressan Faris Al-Maliky |
| collection | DOAJ |
| description | In present work numerical two dimensions, steady, incompressible, turbulent flow past S809 wind turbine airfoil with microtab at 95% of chord length of leading edge in lower surface is analyzed by Fluent (6.2) program for model consists of S809 airfoil without and with microtab at 95% of chord line have height 1.1% and other 2% of chord length undergo to turbulent flow k-. model, the flow has Reynolds number is 106. The results are represented by velocity contour and vector. Aerodynamic coefficients are drawn in graph. The results are showed an increase lift and drag coefficient in existence microtab locate 95% of chord at it's height 1.1% and 2% of chord to range of attack angle (0, 5, 10, 15, 20) degrees. The results compare with experimental data of standard airfoil and existence 1.1% chord length microtab and it is approximately good. Values of lift & drag coefficient are increased for the existence of 1.1% chord length microtab while in case the existence of microtab 2% chord length lift coefficient increased which it's max. increment by 46% while, drag coefficient decreased it's min. increment to be 26% but not full range of attack angle. |
| first_indexed | 2024-03-08T06:10:13Z |
| format | Article |
| id | doaj.art-29281ca8ccba4302a79587ff0c91b47f |
| institution | Directory Open Access Journal |
| issn | 1681-6900 2412-0758 |
| language | English |
| last_indexed | 2024-03-08T06:10:13Z |
| publishDate | 2012-10-01 |
| publisher | Unviversity of Technology- Iraq |
| record_format | Article |
| series | Engineering and Technology Journal |
| spelling | doaj.art-29281ca8ccba4302a79587ff0c91b47f2024-02-04T17:40:16ZengUnviversity of Technology- IraqEngineering and Technology Journal1681-69002412-07582012-10-0130183253326710.30684/etj.30.18.1166155Aerodynamic Characteristics Improving of S809 Airfoil in Wind Turbine with MicrotabRessan Faris Al-MalikyIn present work numerical two dimensions, steady, incompressible, turbulent flow past S809 wind turbine airfoil with microtab at 95% of chord length of leading edge in lower surface is analyzed by Fluent (6.2) program for model consists of S809 airfoil without and with microtab at 95% of chord line have height 1.1% and other 2% of chord length undergo to turbulent flow k-. model, the flow has Reynolds number is 106. The results are represented by velocity contour and vector. Aerodynamic coefficients are drawn in graph. The results are showed an increase lift and drag coefficient in existence microtab locate 95% of chord at it's height 1.1% and 2% of chord to range of attack angle (0, 5, 10, 15, 20) degrees. The results compare with experimental data of standard airfoil and existence 1.1% chord length microtab and it is approximately good. Values of lift & drag coefficient are increased for the existence of 1.1% chord length microtab while in case the existence of microtab 2% chord length lift coefficient increased which it's max. increment by 46% while, drag coefficient decreased it's min. increment to be 26% but not full range of attack angle.https://etj.uotechnology.edu.iq/article_66155_0313bee27887938f4d5d68eb2d2a0fa0.pdfturbulentmicrotab |
| spellingShingle | Ressan Faris Al-Maliky Aerodynamic Characteristics Improving of S809 Airfoil in Wind Turbine with Microtab Engineering and Technology Journal turbulent microtab |
| title | Aerodynamic Characteristics Improving of S809 Airfoil in Wind Turbine with Microtab |
| title_full | Aerodynamic Characteristics Improving of S809 Airfoil in Wind Turbine with Microtab |
| title_fullStr | Aerodynamic Characteristics Improving of S809 Airfoil in Wind Turbine with Microtab |
| title_full_unstemmed | Aerodynamic Characteristics Improving of S809 Airfoil in Wind Turbine with Microtab |
| title_short | Aerodynamic Characteristics Improving of S809 Airfoil in Wind Turbine with Microtab |
| title_sort | aerodynamic characteristics improving of s809 airfoil in wind turbine with microtab |
| topic | turbulent microtab |
| url | https://etj.uotechnology.edu.iq/article_66155_0313bee27887938f4d5d68eb2d2a0fa0.pdf |
| work_keys_str_mv | AT ressanfarisalmaliky aerodynamiccharacteristicsimprovingofs809airfoilinwindturbinewithmicrotab |