A Design Method for Cascades Consisting of Circular Arc Blades with Constant Thickness
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[1] R. I. Lewis,et al. Turbomachinery Performance Analysis , 1996 .
[2] John D Stanitz. Effect of blade-thickness taper on axial-velocity distribution at the leading edge of an entrance rotor-blade row with axial inlet, and the influence of this distribution on alignment of the rotor blade for zero angle of attack , 1953 .
[3] W. B. Roberts. The Effect of Reynolds Number and Laminar Separation on Axial Cascade Performance , 1975 .
[5] J. Katz,et al. Low-Speed Aerodynamics , 1991 .
[6] F. Menter. Two-equation eddy-viscosity turbulence models for engineering applications , 1994 .
[7] B. Lakshminarayana. Fluid dynamics and heat transfer of turbomachinery , 1995 .