Vortex dynamic mechanism of curved blade affecting flow loss in compressor cascade during corner stall process

Author:

Kan Xiaoxu,Wang Songtao,Yang Ling,Zhong Jingjun

Funder

China Postdoctoral Science Foundation

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. Rotational flow through cascades part I. The components of vorticity;Hawthorne;Q. J. Mech. Appl. Math.,1955

2. Rotational flow through cascades part II. The circulation about the cascade;Hawthorne;Q. J. Mech. Appl. Math.,1955

3. Flow visualization in a linear turbine cascade of high performance turbine blades;Wang;J. Turbomach.,1995

4. S. Kang, Investigation of the Three Dimensional Flow within a Compressor Cascade with and without Tip Clearance, Vrije Universiteit Brussel, 1993, pp. I-1–V-44.

5. Numerical-simulation of compressor endwall and casing treatment flow phenomena;Crook;J. Turbomach.,1993

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