Prediction of boundary-layer transition caused by crossflow disturbances

Conference object Japanese OPEN
Nomura, Toshiyuki ; 野村 聡幸 (1999)
  • Publisher: 航空宇宙技術研究所
  • Journal: 航空宇宙技術研究所特別資料=Special Publication of National Aerospace Laboratory 265-269 (issn: 0289-260X)
  • Subject: crossflow disturbance prediction system | 後退円柱 | velocity distribution | 空間増幅 | linear stability analysis | Navier Stokes code | temperature distribution | spatial growth | ナビエ・ストークスコード | 速度分布 | compressible boundary layer | 温度分布 | boudary layer transition | swept cylinder | transition onset location | 線形PSEコード | 境界層遷移予測システム | 遷移開始位置 | sweptback wing | N factor code | 線形安定解析 | 圧縮性境界層 | 横流れ擾乱 | 後退翼 | 超音速輸送機 | linear PSE code | supersonic airplane | parabolized stability equation | N値法コード | 放物型安定方程式
    arxiv: Physics::Fluid Dynamics

A prediction system for boundary layer transition is developed which consists of the Navier-Stokes code computing a compressible boundary layer, the linear PSE (Parabolized Stability Equations) code computing the spatial growth of a disturbance, and the N-factor code in... View more
Share - Bookmark

  • Download from
    JAIRO via JAIRO (Conference object, 1999)
  • Cite this publication