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宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005. :150-155
In small gas turbine engines, the boundary layer separation-reattachment phenomena on low pressure turbine blade surfaces are strongly affected by the upstream wakes at low Reynolds number conditions (O is approximately 10(exp 5)). It is well known t