| Yazarlar (3) |
Tuğrul Oktay
Erciyes Üniversitesi, Türkiye |
Dr. Öğr. Üyesi Öztürk Özdemir KANAT
Kastamonu Üniversitesi, Türkiye |
|
Aziz Ceyhan
|
| Özet |
| In this conference article improvement of wingtip vortices with the active flow controller with 6 blowing points is analyzed using the Fluent Program for aircraft with a NACA 2415 wing. To control the countercurrent vortices on the wing, blowers are positioned at points of 0.3 b, 0.6 b, and 0.9 b (ie b is the half wing span) on each side of the wing and half width of the chords. Effect of different pressure discharge and angle of attack are considered. Due to the several blowing points at each side of the wing, more aerodynamic fines coefficient improvement is obtained with respect to the active flow controller having single blower at each side of the wing. |
| Anahtar Kelimeler |
| Bildiri Türü | Tebliğ/Bildiri |
| Bildiri Alt Türü | Tam Metin Olarak Yayınlanan Tebliğ (Uluslararası Kongre/Sempozyum) |
| Bildiri Niteliği | Alanında Hakemli Uluslararası Kongre/Sempozyum |
| Bildiri Dili | İngilizce |
| Kongre Adı | 8th International Advanced Technologies Symposium |
| Kongre Tarihi | 19-10-2017 / 22-10-2017 |
| Basıldığı Ülke | Türkiye |
| Basıldığı Şehir | Elazığ |
