Aerodynamic Performance Improvement with Morphing Winglet Design
Yıl: 2021 Cilt: 5 Sayı: 1 Sayfa Aralığı: 16 - 21 Metin Dili: İngilizce DOI: 10.30518/jav.884721 İndeks Tarihi: 24-11-2021
Aerodynamic Performance Improvement with Morphing Winglet Design
Öz: The aim of this study is to reduce unnecessary lift and minimize drag at the same time when the aircraft reaches a certain speed level by using the active morphing method during flight. In this study, the flight performance was improved by designing a morphing winglet. Aerodynamic analysis of the wing in flat level flight at speeds of 15, 20 and 25 m / s has been performed. Morphing winglet of the wing was analyzed separately at 0-20-45-60-75 degree toe angles at speeds of 10-15-20-25-30 m / s. Optimum parameters have been determined to achieve maximum lift and minimum drag.
Anahtar Kelime: Belge Türü: Makale Makale Türü: Araştırma Makalesi Erişim Türü: Erişime Açık
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| APA | uzun m, ÇOBAN S (2021). Aerodynamic Performance Improvement with Morphing Winglet Design. , 16 - 21. 10.30518/jav.884721 |
| Chicago | uzun metin,ÇOBAN SEZER Aerodynamic Performance Improvement with Morphing Winglet Design. (2021): 16 - 21. 10.30518/jav.884721 |
| MLA | uzun metin,ÇOBAN SEZER Aerodynamic Performance Improvement with Morphing Winglet Design. , 2021, ss.16 - 21. 10.30518/jav.884721 |
| AMA | uzun m,ÇOBAN S Aerodynamic Performance Improvement with Morphing Winglet Design. . 2021; 16 - 21. 10.30518/jav.884721 |
| Vancouver | uzun m,ÇOBAN S Aerodynamic Performance Improvement with Morphing Winglet Design. . 2021; 16 - 21. 10.30518/jav.884721 |
| IEEE | uzun m,ÇOBAN S "Aerodynamic Performance Improvement with Morphing Winglet Design." , ss.16 - 21, 2021. 10.30518/jav.884721 |
| ISNAD | uzun, metin - ÇOBAN, SEZER. "Aerodynamic Performance Improvement with Morphing Winglet Design". (2021), 16-21. https://doi.org/10.30518/jav.884721 |
| APA | uzun m, ÇOBAN S (2021). Aerodynamic Performance Improvement with Morphing Winglet Design. Journal of aviation (Online), 5(1), 16 - 21. 10.30518/jav.884721 |
| Chicago | uzun metin,ÇOBAN SEZER Aerodynamic Performance Improvement with Morphing Winglet Design. Journal of aviation (Online) 5, no.1 (2021): 16 - 21. 10.30518/jav.884721 |
| MLA | uzun metin,ÇOBAN SEZER Aerodynamic Performance Improvement with Morphing Winglet Design. Journal of aviation (Online), vol.5, no.1, 2021, ss.16 - 21. 10.30518/jav.884721 |
| AMA | uzun m,ÇOBAN S Aerodynamic Performance Improvement with Morphing Winglet Design. Journal of aviation (Online). 2021; 5(1): 16 - 21. 10.30518/jav.884721 |
| Vancouver | uzun m,ÇOBAN S Aerodynamic Performance Improvement with Morphing Winglet Design. Journal of aviation (Online). 2021; 5(1): 16 - 21. 10.30518/jav.884721 |
| IEEE | uzun m,ÇOBAN S "Aerodynamic Performance Improvement with Morphing Winglet Design." Journal of aviation (Online), 5, ss.16 - 21, 2021. 10.30518/jav.884721 |
| ISNAD | uzun, metin - ÇOBAN, SEZER. "Aerodynamic Performance Improvement with Morphing Winglet Design". Journal of aviation (Online) 5/1 (2021), 16-21. https://doi.org/10.30518/jav.884721 |
