Araştırma Makalesi/Research Article DOI: 10.30518/jav. 633775
Yazarlar (4)
Prof. Dr. Mehmet Mustafa ÖNAL Türkiye
Sezer Çoban
Ahmet Yapici
Dr. Öğr. Üyesi Hasan Hüseyin Bilgiç Kırşehir Ahi Evran Üniversitesi
| Makale Türü | Özgün Makale (Uluslararası alan indekslerindeki dergilerde yayınlanan tam makale) | ||
| Dergi Adı | Journal of Aviation | ||
| Makale Dili | – | Basım Tarihi | 01-2019 |
| Cilt / Sayı / Sayfa | 3 / 2 / 106–112 | DOI | 10.30518/jav |
| Makale Linki | https://www.researchgate.net/profile/Hasan-Bilgic/publication/338164601_Dikey_Inis_Kalkis_Yapabilen_Bir_IHA'nin_Azami_Menzili_ve_Asgari_Guc_Gereksinimi_Icin_En_Uygun_Ucus_Parametrelerinin_Belirlenmesi/links/61505f55522ef665fb5f3c54/Dikey-Inis-Kalkis- | ||
| UAK Araştırma Alanları |
Betonarme Yapılar
|
||
| Özet |
| When designing unmanned aerial vehicles (UAVs), it is taken into consideration that certain features are met. In some UAVs, models are designed according to the maximum speeds that can be reached, while in others, they are designed according to the maximum lifting forces. In this study, flight parameters were calculated by aerodynamic analysis performed in an analysis program in order to reach the maximum range of a designed UAV and then the UAV was produced. During the aerodynamic analysis, first the wing profile and then the whole body were analyzed. As a result of the analyzes, the most suitable angle of attack for minimum power requirement and maximum range was obtained as 12 and 8, respectively. |
| Anahtar Kelimeler |