The Effects of Radially Distorted Incident Flow on Performance of Axial-Flow Fans With Forward-Skewed Blades

In this study, experiments and numerical simulations were carried out to evaluate the effects of radially distorted incident flow on the performance of axial-flow fans, which were equipped with three kinds of forward-skewed blades. Loss coefficient and velocity components at exit section as well as overall performance are discussed, both at the design point and the lower mass flow rate point. Furthermore, rotating stall was also observed by use of three dynamic pressure sensors. All results reveal that there are beneficial effects of forward-skewed blades on the fan performance, but the fan performance and its unsteady aerodynamic characteristics are quite affected by the radially distorted incident flow.

[1]  Robert J. Lubick,et al.  Inlet-air distortion effects on stall, surge, and acceleration margin of a turbojet engine equipped with variable compressor inlet guide vanes , 1955 .

[2]  James D. Paduano,et al.  Rotating Stall Control in a High-Speed Stage With Inlet Distortion: Part I—Radial Distortion , 1999 .

[3]  Detlev G. Kröger,et al.  Effect of inlet flow distortions on fan performance in forced draught air-cooled heat exchangers , 1995 .

[4]  David C. Wilcox,et al.  Comparison of two-equation turbulence models for boundary layers with pressure gradient , 1993 .

[5]  C. Hah,et al.  Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor , 1998 .

[6]  Dirk C. Leinhos,et al.  The Influence of Transient Inlet Distortions on the Instability Inception of a Low Pressure Compressor in a Turbofan Engine , 2001 .

[7]  Leroy H. Smith,et al.  Sweep and Dihedral Effects in Axial-Flow Turbomachinery , 1963 .

[8]  Rodrick V. Chima,et al.  A Three-Dimensional Unsteady CFD Model of Compressor Stability , 2013 .

[9]  M. G. Beiler,et al.  Computation and Measurement of the Flow in Axial Flow Fans With Skewed Blades , 1999 .

[10]  Y. Carels,et al.  Influence Of Dihedral on the Secondary Flow in a Two-Dimensional Compressor Cascade , 1984 .

[11]  F. Menter Performance of popular turbulence model for attached and separated adverse pressure gradient flows , 1992 .

[12]  Th. Carolus,et al.  Skewed Blades in Low Pressure Fans: A Survey of Noise Reduction Mechanisms , 1997 .

[13]  Kwang-Yong Kim,et al.  Effects of Inflow Distortion due to Hub Cap's Shape on the Performance of Axial Flow Fan , 2008 .

[14]  F. A. E. Breugelmans,et al.  Comparison of Sweep and Dihedral Effects on Compressor Cascade Performance , 1997 .

[16]  Nicholas A. Cumpsty,et al.  The Use of Sweep and Dihedral in Multistage Axial Flow Compressor Blading—Part I: University Research and Methods Development , 2002 .