Numerical optimization of a stator blade to enhance aerodynamic performance in a transonic fan stage-Reference-Cited by-同舟云学术

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Numerical optimization of a stator blade to enhance aerodynamic performance in a transonic fan stage

Published:2024-01 Issue: Volume:103 Page:163-181
ISSN:0997-7546
Container-title:European Journal of Mechanics - B/Fluids
language:en
Short-container-title:European Journal of Mechanics - B/Fluids

Author:

Park Kun Sung,Zamiri Ali,Choi Minsuk,Lee Byung Ju,Chung Jin Taek

Funder

Ministry of Education

Ministry of Trade, Industry and Energy

National Research Foundation of Korea

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Mathematical Physics

Reference44 articles.

1. Unsteady flows in a single-stage row, axial-flow fan stator;Hathaway;NASA Tech. Memo.,1987

2. Experimental study of a high- throughflow transonic axial compressor stage;Wennerstrom;J. Eng. Gas Turbines Power,1984

3. N.A. Cumpsty, Compressor aerodynamics, (Book), 2004.

4. D. Japikse, Introduction to turbomachinery, (Book), Concepts ETI, Inc., 1994.

5. Some aspects of the transonic compressor tandem design;Hergt;J. Turbomach.,2019

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1. Optimization of an axial-flow mine ventilation fan based on effects of design parameters;Results in Engineering;2024-03

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