並列タイトル等Turbulence Models for Transonic Flows with Separation
タイトル(掲載誌)航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-10
一般注記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
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43336&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ