Fujitsu Limited
National Aerospace Laboratory
National Aerospace Laboratory
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory(NAL)
雑誌名
航空宇宙技術研究所特別資料
雑誌名(英)
Special Publication of National Aerospace Laboratory SP-10
巻
10
ページ
39 - 44
発行年
1989-11
抄録（英）
Computation of 3-D transonic viscous flows around the ONERA-M6 wing is performed by using several turbulence models with our improved Harten-Yee TVD scheme. The models used here are the Baldwin-Lomax model, Subgrid-Scale (SGS) model and Jones-Launder (k-epsilon)-model, and the test condition is a flow with the interaction of shock wave and boundary layer under the large separation As the result, it is concluded that the SGS and (k-epsilon) models work well compared with the Baldwin-Lomax model, and that the physical phenomena such as the interaction of shock wave and boundary layer numerically captured are qualitatively correct when the pressure distributions agree with experimental ones.
剥離を含む遷音速流のための乱流モデルの検討
nalsp0010007.pdf
(647.3KB)
