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弦向缝隙叶栅对边界层分离的控制
引用本文:曹军 沈炳正. 弦向缝隙叶栅对边界层分离的控制[J]. 空气动力学学报, 1993, 11(4): 445-450
作者姓名:曹军 沈炳正
作者单位:中国空气动力研究与发展中心,上海机械学院 四川绵阳 621000,上海 200093
摘    要:本文提出了一种在S1流面上进行势流与粘性流迭代求解弦向缝隙叶栅流场的计算方法,将S1流面上势流方程组的解与经I11ingworth-Stewartson变换后的边界层方程结合起来联立求解弦向缝隙叶栅流场。计算值同实验结果相当吻合,在正大攻角时,向缝隙叶栅能效地控制边界层分离。

关 键 词:叶栅流动 边界层分离 数值计算

Boundary Layer Separation Control by Cascade with Chordwise-Split Blades
Cao Jun. Boundary Layer Separation Control by Cascade with Chordwise-Split Blades[J]. Acta Aerodynamica Sinica, 1993, 11(4): 445-450
Authors:Cao Jun
Affiliation:Cao Jun (China Aerodynamics Research and Development Center)Shen Bingzheng (Shanghai Institute of Mechanical Engineering)
Abstract:This paper sets faith a method of calculation by iterating the potential flow and viscous flow on S1 stream-sheet to solve the flowfield of the cascade with chordwise-split blades. It can get the solution of the flowfield of the cascade with chordwise-split blades by means of combining the potential equations on S1 stream-sheet and boundary layer equations by Illingworth-Stewartson transformation, the agreement between the calculation and experiment data is good. The cascade with chordwise-split blades can effectively control the boundary layer separation at positive angles of attack.
Keywords:cascade flow   boundary layer separation   numerical computation.  
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