Parallel computation of flows around flapping airfoils in biplane configuration
International Parallel Computational Fluid Dynamics Conference, KANSAI SCI CITY, Japonya, 20 - 22 Mayıs 2002, ss.523-530, (Tam Metin Bildiri)
- Yayın Türü: Bildiri / Tam Metin Bildiri
- Doi Numarası: 10.1016/b978-044450680-1/50066-8
- Basıldığı Şehir: KANSAI SCI CITY
- Basıldığı Ülke: Japonya
- Sayfa Sayıları: ss.523-530
- Orta Doğu Teknik Üniversitesi Adresli: Evet
Özet
Unsteady, laminar flows over flapping airfoils in biplane configuration are computed on overset grids. The overset grid solutions are obtained in parallel in a cluster environment. It is shown that airfoils in biplane configuration and oscillating in pitch and plunge with a proper phase shift between them enhance the thrust production significantly.