A CFD analysis of NACA 0015 airfoil as a horizontal stabilizer with gap length variations
The horizontal stabilizer is an important device which stabilize in the longitudinal direction is an important device for aviation. It also controls the pitching nose through the variation of elevator deflection angle. This work is to relate the lift coefficient with elevator deflection angle. The a...
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| Format: | Article |
| Language: | English |
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University of Muhammadiyah Malang
2023-06-01
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| Series: | JEMMME (Journal of Energy, Mechanical, Material, and Manufacturing Engineering) |
| Subjects: | |
| Online Access: | https://ejournal.umm.ac.id/index.php/JEMMME/article/view/26425 |
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| author | Gunawan Nugroho Herman Sasongko Mohammad Adenan Sarwono Heru Mirmanto |
| author_facet | Gunawan Nugroho Herman Sasongko Mohammad Adenan Sarwono Heru Mirmanto |
| author_sort | Gunawan Nugroho |
| collection | DOAJ |
| description | The horizontal stabilizer is an important device which stabilize in the longitudinal direction is an important device for aviation. It also controls the pitching nose through the variation of elevator deflection angle. This work is to relate the lift coefficient with elevator deflection angle. The applied horizontal stabiliser is a plain flap with the gap length of 1.75%, 2% and 2.25% w.r.t. chord length. Results show that higher elevator deflection angle increases lift coefficient. For the 2 degree angle of attack and 20 degree of elevetor deflection angle, the lift coefficient is 0.93 (gap length 1.75%). Moreover, the lift coefficient is 1.83 for 10 degree horizontal stabiliser (gap length 2%). |
| format | Article |
| id | doaj-art-983b2fe39838480e8f9a32c18fee3ac4 |
| institution | Kabale University |
| issn | 2541-6332 2548-4281 |
| language | English |
| publishDate | 2023-06-01 |
| publisher | University of Muhammadiyah Malang |
| record_format | Article |
| series | JEMMME (Journal of Energy, Mechanical, Material, and Manufacturing Engineering) |
| spelling | doaj-art-983b2fe39838480e8f9a32c18fee3ac42025-01-21T05:02:28ZengUniversity of Muhammadiyah MalangJEMMME (Journal of Energy, Mechanical, Material, and Manufacturing Engineering)2541-63322548-42812023-06-0172758210.22219/jemmme.v7i2.2642524242A CFD analysis of NACA 0015 airfoil as a horizontal stabilizer with gap length variationsGunawan Nugroho0Herman Sasongko1Mohammad Adenan2Sarwono3Heru Mirmanto4Institut Teknologi Sepuluh NopemberInstitut Teknologi Sepuluh NopemberInstitut Teknologi Sepuluh NopemberInstitut Teknologi Sepuluh NopemberInstitut Teknologi Sepuluh NopemberThe horizontal stabilizer is an important device which stabilize in the longitudinal direction is an important device for aviation. It also controls the pitching nose through the variation of elevator deflection angle. This work is to relate the lift coefficient with elevator deflection angle. The applied horizontal stabiliser is a plain flap with the gap length of 1.75%, 2% and 2.25% w.r.t. chord length. Results show that higher elevator deflection angle increases lift coefficient. For the 2 degree angle of attack and 20 degree of elevetor deflection angle, the lift coefficient is 0.93 (gap length 1.75%). Moreover, the lift coefficient is 1.83 for 10 degree horizontal stabiliser (gap length 2%).https://ejournal.umm.ac.id/index.php/JEMMME/article/view/26425horizontal stabilizerelevator deflection angleplain flaplift coefficient |
| spellingShingle | Gunawan Nugroho Herman Sasongko Mohammad Adenan Sarwono Heru Mirmanto A CFD analysis of NACA 0015 airfoil as a horizontal stabilizer with gap length variations JEMMME (Journal of Energy, Mechanical, Material, and Manufacturing Engineering) horizontal stabilizer elevator deflection angle plain flap lift coefficient |
| title | A CFD analysis of NACA 0015 airfoil as a horizontal stabilizer with gap length variations |
| title_full | A CFD analysis of NACA 0015 airfoil as a horizontal stabilizer with gap length variations |
| title_fullStr | A CFD analysis of NACA 0015 airfoil as a horizontal stabilizer with gap length variations |
| title_full_unstemmed | A CFD analysis of NACA 0015 airfoil as a horizontal stabilizer with gap length variations |
| title_short | A CFD analysis of NACA 0015 airfoil as a horizontal stabilizer with gap length variations |
| title_sort | cfd analysis of naca 0015 airfoil as a horizontal stabilizer with gap length variations |
| topic | horizontal stabilizer elevator deflection angle plain flap lift coefficient |
| url | https://ejournal.umm.ac.id/index.php/JEMMME/article/view/26425 |
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