Research on the lean and swept optimization of a single stage axial compressor-Reference-Cited by-同舟云学术

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Research on the lean and swept optimization of a single stage axial compressor

Published:2021-01-01 Issue:1 Volume:15 Page:142-163
ISSN:1994-2060
Container-title:Engineering Applications of Computational Fluid Mechanics
language:en
Short-container-title:Engineering Applications of Computational Fluid Mechanics

Author:

Wang Zhongyi¹,Qu Feng¹,Wang Yanhua¹,Luan Yigang¹,Wang Meng¹

Affiliation:

1. College of Power and Energy Engineering, Harbin Engineering University, Harbin, People’s Republic of China

Funder

National Natural Science Foundation of China

National Science and Technology Major Project

Outstanding Youth Foundation of Heilongjiang Province

Publisher

Informa UK Limited

Subject

Modeling and Simulation,General Computer Science

Link

https://www.tandfonline.com/doi/pdf/10.1080/19942060.2020.1862708

Reference29 articles.

1. Experimental and computational fluid dynamics-based numerical simulation of using natural gas in a dual-fueled diesel engine

2. Aerodynamics of swept and leaned transonic compressor-rotors

3. Aerodynamic sweeping study and design for transonic compressor rotor blades

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1. Prescreening surrogate-model-assisted multi-objective aerodynamic optimization design of highly loaded axial compressor in heavy-duty gas turbine;Applied Thermal Engineering;2024-10

2. Prediction of Aerodynamic Forces at the Tip of the Compressor Blades Based on Multi-scale 1DCNN Combined with CBAM;Thin-Walled Structures;2024-10

3. Effect of leaned blades on the aerodynamic performance of contra-rotating open rotor;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-08-22

4. Aerodynamic performance and flow optimization of axial fan based on the neural network and genetic algorithm;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2024-07-26

5. Unsteady Analysis of Secondary Vortex Formations Within An Axial Compressor Stage with Tandem Rotor;Arabian Journal for Science and Engineering;2024-07-16

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