Experimental Study on the Aerodynamic Performance of Swept Curved Blade

Author:

ZHAO Gui-jie,CHEN Fu,SONG Yan-ping,WANG Zhong-qi

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference6 articles.

1. Hah C. Aerodynamic lean and sweep for improvements in compressor performances[R]. Von Karman Institute for Fluid Dynamics, Lecture Series 1999-02, Turbomachinery Blade Design Systems, 1999.

2. Influence of dihedral on the secondary flow in a two dimensional compressor cascade[J];Breugelmans;ASME Journal of Engineering for Gas Turbine and Power,1984

3. Weingold H D, Neubert R J, Behlke R F, et al. Reduction of compressor stator endwall losses through the use of bowed stators[R]. ASME Paper 95-GT-380, 1995.

4. Stator endwall leading edge sweep and hub shroud influence on compressor performance[J];Tweedt;ASME Journal of Turbomachinery,1986

5. Comparison of sweep and dihedral effects on compressor cascade performance[J];Sasaki;ASME Journal of Turbomachinery,1998

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