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机译:涡旋脱落在薄膜冷却过程中的影响
Department of Applied Mechanics and Engineering School of Aeronautics and Astronautics Sun Yat-sen University Guangzhou China;
Department of Applied Mechanics and Engineering School of Aeronautics and Astronautics Sun Yat-sen University Guangzhou China;
Department of Civil and Environmental Engineering The Hong Kong Polytechnic University Hong Kong China;
Department of Applied Mechanics and Engineering School of Aeronautics and Astronautics Sun Yat-sen University Guangzhou China;
Department of Applied Mechanics and Engineering School of Aeronautics and Astronautics Sun Yat-sen University Guangzhou China;
机译:具有新颖脱落准则的离散涡旋方法,用于不定常翼型流动且具有间歇性前沿涡旋脱落
机译:交错排列的螺旋形固体翅片管束的涡旋脱落特性(由管排列引起的涡旋脱落图案)
机译:螺旋固体翅片管捆扎交错布置的涡流脱落特性(管安排引起的涡旋脱落图)
机译:螺旋桨叶尖涡旋,尾缘涡旋和切旋涡旋相互作用引起的非定常压力场
机译:拉格朗日的可视化和圆柱尾流中涡旋脱落时间的实时识别
机译:通过筒绕筒中的扑振标志装置直接缩放涡流脱落
机译:涡流循环对湍流边界层中单个膜冷却孔和一排膜冷却孔的注入剂的影响,第2部分:在涡流上冲下方注入