Effect of Turning Angle on Flow Field Performance of Linear Bowed Stator in Compressor at Low Mach Number

Author:

ZHANG Yong-jun,CHEN Fu,FENG Guo-tai,SU Jie-xian

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference9 articles.

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2. 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 952GT2380, 1995.

3. Experimental study on the aerodynamic performance of swept-Curved blade[J];Zhao;Chinese Journal of Aeronautics,2004

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

5. Sweep and dihedral effects in axial-flow turbomachinery[J];Smith;Journal of Basic Engineering,1963

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