Aerodynamic Optimization of a UAV Wing subject to Weight, Geometric, Root Bending Moment, and Performance Constraints
Yazarlar (2)
Durmuş Sinan Körpe
Türk Hava Kurumu Üniversitesi, Türkiye
Türk Hava Kurumu Üniversitesi, Türkiye
Dr. Öğr. Üyesi Öztürk Özdemir KANAT Kastamonu Üniversitesi, Türkiye
| Makale Türü |
Özgün Makale
(SSCI, AHCI, SCI, SCI-Exp dergilerinde yayınlanan tam makale)
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| Dergi Adı | International Journal of Aerospace Engineering (Q3) | ||
| Dergi ISSN | 1687-5966 Wos Dergi Scopus Dergi | ||
| Dergi Tarandığı Indeksler | SCI-Expanded | ||
| Makale Dili | İngilizce | Basım Tarihi | 10-2019 |
| Kabul Tarihi | – | Yayınlanma Tarihi | 16-10-2019 |
| Cilt / Sayı / Sayfa | 2019 / 1 / 1–14 | DOI | 10.1155/2019/3050824 |
| Makale Linki | https://www.hindawi.com/journals/ijae/2019/3050824/ | ||
| UAK Araştırma Alanları |
Aerodinamik
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| Özet |
| In this study, the optimization of a low‐speed wing with functional constraints is discussed. The aerodynamic analysis tool developed by the coupling of the numerical nonlinear lifting‐line method to Xfoil is used to obtain lift and drag coefficients of the baseline wing. The outcomes are compared with the results of the solver based on the nonlinear lifting‐line theory implemented into XLFR5 and the transition shear stress transport model implemented into ANSYS‐Fluent. The agreement between the results at the low and moderate angle of attack values is observed. The sequential quadratic programming algorithm of the MATLAB optimization toolbox is used for the solution of the constrained optimization problems. Three different optimization problems are solved. In the first problem, the maximization of is the objective function, while level flight condition at maximum is defined as a constraint. The … |
| Anahtar Kelimeler |
BM Sürdürülebilir Kalkınma Amaçları
| Atıf Sayıları | |
| Web of Science | 8 |
| Scopus | 10 |
| Google Scholar | 21 |