Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds
An aerodynamic technique to calculating lift and drag coefficients is one of the required instruments in the wing design process. During the last decades, several tools and software have been developed according to aero-dynamics and numerical methods. Nowadays, aeronautical architecture requires man...
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| Format: | Article |
| Language: | English |
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Çanakkale Onsekiz Mart University
2022-12-01
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| Series: | Journal of Advanced Research in Natural and Applied Sciences |
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| Online Access: | https://dergipark.org.tr/en/download/article-file/2236420 |
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| author | Sinan Fidan Satılmış Ürgün Mert Gökdemir |
| author_facet | Sinan Fidan Satılmış Ürgün Mert Gökdemir |
| author_sort | Sinan Fidan |
| collection | DOAJ |
| description | An aerodynamic technique to calculating lift and drag coefficients is one of the required instruments in the wing design process. During the last decades, several tools and software have been developed according to aero-dynamics and numerical methods. Nowadays, aeronautical architecture requires many calculations. Today’s techno-logists use a variety of simulation techniques to avoid a expensive model testing. This paper explains how wing profiles can be modelled using ANSYS Fluent and tested by low-speed tests considering experimental literature re-sults. With the selected wing profile, the geometry is shaped in two dimensions and designed in three dimensions. Computational fluid dynamics (CFD) was adopted as the method for studying wing profiles. Wing profiles created at 0 to 20-degree attack angles are calculated in the simulation area equal to the actual wind tunnel scale, and equations are solved using the RNG k-Epsilon turbulence model. The process of developing the grids was realized with Ansys Mesher software. The solution stage and the result show operations were carried out with the CFD Post software. The study of the low velocity and high transport wing profiles, the drag coefficient, the lift coefficient, and the effect on the lift-drag ratio were studied using a numerical procedure. After determining the high efficiency of wing profi-les, production of a selected profile began with a static examination. |
| format | Article |
| id | doaj-art-98923ae220b94212897f132df63d6367 |
| institution | Kabale University |
| issn | 2757-5195 |
| language | English |
| publishDate | 2022-12-01 |
| publisher | Çanakkale Onsekiz Mart University |
| record_format | Article |
| series | Journal of Advanced Research in Natural and Applied Sciences |
| spelling | doaj-art-98923ae220b94212897f132df63d63672025-02-05T17:57:35ZengÇanakkale Onsekiz Mart UniversityJournal of Advanced Research in Natural and Applied Sciences2757-51952022-12-018460061310.28979/jarnas.1069147453Comparative analysis and manufacturing of airfoil structures suitable for use at low speedsSinan Fidan0https://orcid.org/0000-0003-4385-4981Satılmış Ürgün1https://orcid.org/0000-0003-3889-6909Mert Gökdemir2https://orcid.org/0000-0002-2047-1331KOCAELI UNIVERSITY, FACULTY OF AERONAUTICS AND ASTRONAUTICSKOCAELI UNIVERSITY, FACULTY OF AERONAUTICS AND ASTRONAUTICSKOCAELİ ÜNİVERSİTESİ, HAVACILIK VE UZAY BİLİMLERİ FAKÜLTESİAn aerodynamic technique to calculating lift and drag coefficients is one of the required instruments in the wing design process. During the last decades, several tools and software have been developed according to aero-dynamics and numerical methods. Nowadays, aeronautical architecture requires many calculations. Today’s techno-logists use a variety of simulation techniques to avoid a expensive model testing. This paper explains how wing profiles can be modelled using ANSYS Fluent and tested by low-speed tests considering experimental literature re-sults. With the selected wing profile, the geometry is shaped in two dimensions and designed in three dimensions. Computational fluid dynamics (CFD) was adopted as the method for studying wing profiles. Wing profiles created at 0 to 20-degree attack angles are calculated in the simulation area equal to the actual wind tunnel scale, and equations are solved using the RNG k-Epsilon turbulence model. The process of developing the grids was realized with Ansys Mesher software. The solution stage and the result show operations were carried out with the CFD Post software. The study of the low velocity and high transport wing profiles, the drag coefficient, the lift coefficient, and the effect on the lift-drag ratio were studied using a numerical procedure. After determining the high efficiency of wing profi-les, production of a selected profile began with a static examination.https://dergipark.org.tr/en/download/article-file/2236420airfoilansysnacacfdlift |
| spellingShingle | Sinan Fidan Satılmış Ürgün Mert Gökdemir Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds Journal of Advanced Research in Natural and Applied Sciences airfoil ansys naca cfd lift |
| title | Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds |
| title_full | Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds |
| title_fullStr | Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds |
| title_full_unstemmed | Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds |
| title_short | Comparative analysis and manufacturing of airfoil structures suitable for use at low speeds |
| title_sort | comparative analysis and manufacturing of airfoil structures suitable for use at low speeds |
| topic | airfoil ansys naca cfd lift |
| url | https://dergipark.org.tr/en/download/article-file/2236420 |
| work_keys_str_mv | AT sinanfidan comparativeanalysisandmanufacturingofairfoilstructuressuitableforuseatlowspeeds AT satılmısurgun comparativeanalysisandmanufacturingofairfoilstructuressuitableforuseatlowspeeds AT mertgokdemir comparativeanalysisandmanufacturingofairfoilstructuressuitableforuseatlowspeeds |