Transonic wing flows using an Euler/Navier-Stokes zonal approach
Journal of Aircraft, cilt.24, sa.1, ss.17-24, 1987 (Scopus)
- Yayın Türü: Makale / Tam Makale
- Cilt numarası: 24 Sayı: 1
- Basım Tarihi: 1987
- Doi Numarası: 10.2514/3.45405
- Dergi Adı: Journal of Aircraft
- Derginin Tarandığı İndeksler: Scopus
- Sayfa Sayıları: ss.17-24
- Ankara Yıldırım Beyazıt Üniversitesi Adresli: Hayır
Özet
Transonic flowfields about wing geometries are computed using an Euler/Navier-Stokes approach in which the flowfield is divided into several zones. Wind-tunnel wall effects are modeled easily and accurately with the new grid-zoning algorithm because the wind-tunnel grid is constructed as an exact subset of the corresponding free-air grid. Solutions are obtained that are in good agreement with experiment, including cases with significant wind-tunnel wall effects and shock-induced separation on the upper wing surface. © American Institute of Aeronautics and Astronautics, Inc., 1986.