Experimental study of sweepand dihedral effects on compressor cascade performance

ETC 2005 - 6th Conference on Turbomachinery: Fluid Dynamics and Thermodynamics

Volumn , Issue , 2005, Pages

  Song, Yanping ^a   Zhao, Guijie ^a   Chen, Fu ^a   Wang, Zhongqi ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FLOW SEPARATION; SAILING VESSELS; THERMODYNAMICS;

COMPRESSOR CASCADE PERFORMANCE; DIFFUSION FACTOR; END-WALL BOUNDARY LAYERS; LINEAR COMPRESSORS; LOW-ENERGY FLUIDS; OPTIMAL MATCHING; SURFACE STATIC PRESSURE; THREE DIMENSIONAL EFFECT;

DIFFUSION IN LIQUIDS;

EID: 84925431129     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

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2. V. Gümmer, U. Wenger, H-P Kau. Using Sweep and Dihedral to Control Three-Dimensional Flow in Transonic Stators of Axial Compressor. Journal of Turbomachinery. 123(1): 40-48, 2001
3. C. Hah. Aerodynamic Lean and Sweep for Improvements in Compressor Performances. Von Karman Institute for Fluid Dynamics, Turbomachinery Blade Design Systems, Feb. 8-12, 1999
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7. L. H. Smith, H. Yeh. Sweep and Dihedral Effects in Axial-Flow Turbomachinery. Journal of Basic Engineering, 1963, 85: 401-414
8. D. L. Tweedt, T. H. Okiishi and M. D. Hathaway. Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance, ASME Journal of Turbomachinery, Vol. 108 pp. 224-232, 1986
9. Wang Zhongqi, Three-dimensional Theory and Design Method of Bowed Twisted Blade and Its Application to Turbomachines. Turbomachinery Blade Design System, VKI, LS 1999-02
10. Wei Binghai, Wu Keqi. Review on the Research of High Performance Skew-Swept Blades and Its Influence on Inner Flow. FLUID MACHINERY, Vol.29, No.1: 31-34, 2001
11. H. D. Weingold, R. J. Neubert, R. F. Behlke and G. E. Potter. Reduction of Compressor Stator Endwall Losses Through the Use of Bowed Stators, ASME Paper No. 95-GT-380, 1995