Blade bowing effects on radial equilibrium of inlet flow in axial compressor cascades-Reference-Cited by-同舟云学术

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Blade bowing effects on radial equilibrium of inlet flow in axial compressor cascades

Published:2017-10 Issue:5 Volume:30 Page:1651-1659
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

XU Han,CHANG Hao,JIN Donghai,GUI Xingmin

Funder

National Natural Science Foundation of China

National Basic Research Program of China

Beijing Natural Science Foundation

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference20 articles.

1. A new method of profiling the guide vane cascades of turbine stages with small diameter-span ratio;Deich;Teploenegetika,1962

2. Influence of dihedral on the secondary flow in a two-dimensional compressor cascade;Breugelmans;J Eng Gas Turb Power,1984

3. Shang E, Wang ZQ, Su JX. The experimental investigations on the compressor cascades with leaned and curved blade. Proceeding of the ASME 1993 international gas turbine and aeroengine congress and exposition; 1993 May 24–27; Cincinnati, Ohio, USA. New York:ASME;1993.

4. Bowed stators: An example of CFD applied to improve multistage compressor efficiency;Weingold;J Turbomach,1997

5. Performance of strongly bowed stators in a four-stage high-speed compressor;Fischer;J Turbomach,2004

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4. Transient Performance Simulation of Gas Turbine Engine Based on Through-Flow Method and Experimental Verification;Journal of Engineering for Gas Turbines and Power;2023-12-26

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