@techreport{oai:jaxa.repo.nii.ac.jp:00043336,
 author = {高倉, 葉子 and 小川, 哲 and 石黒, 登美子 and Takakura, Yoko and Ogawa, Satoru and Ishiguro, Tomiko},
 month = {Nov},
 note = {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., 資料番号: NALSP0010007, レポート番号: NAL SP-10},
 title = {剥離を含む遷音速流のための乱流モデルの検討},
 year = {1989}
}