Research on aerodynamic optimization design method and flow mechanism of a high-subsonic compressor cascade-Reference-Cited by-同舟云学术

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Research on aerodynamic optimization design method and flow mechanism of a high-subsonic compressor cascade

Published:2022-01-20 Issue:1 Volume:16 Page:316-334
ISSN:1994-2060
Container-title:Engineering Applications of Computational Fluid Mechanics
language:en
Short-container-title:Engineering Applications of Computational Fluid Mechanics

Author:

Huang Song¹²³,Lu Xingen¹²³,Han Ge¹²³,Zhao Shengfeng¹²³,Zhou Chuangxin¹²³,Yang Chengwu¹²³

Affiliation:

1. Key Laboratory of Light-duty Gas-turbine, IET, CAS, Beijing, People’s Republic of China

2. University of Chinese Academy of Sciences, CAS, Beijing, People’s Republic of China

3. Innovation Academy for Light-duty Gas Turbine, CAS, Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

Civil Aircraft Scientific Research Project of China

National Major Science and Technology Projects of China

Publisher

Informa UK Limited

Subject

Modeling and Simulation,General Computer Science

Link

https://www.tandfonline.com/doi/pdf/10.1080/19942060.2021.2020170

Reference47 articles.

1. A numerical and experimental study on the energy efficiency of a regenerative Heat and Mass Exchanger utilizing the counter-flow Maisotsenko cycle

2. Aerodynamic Design Optimization of an Axial Flow Compressor Stator Using Parameterized Free-Form Deformation

3. Tackling Highly Constrained Design Problems: Efficient Optimisation of a Highly Loaded Transonic Compressor

4. The Development of a Second-Generation of Controlled Diffusion Airfoils for Multistage Compressors

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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. Integrated optimization of a turbine stage at a low Reynolds number via NURBS surface and machine learning;Energy;2024-05

3. Extraction of geometric features and analysis of flow mechanism of high loaded compressor airfoils at low Reynolds number;Physics of Fluids;2024-03-01

4. Control of shock–boundary layer interaction in a transonic compressor cascade via heat transfer at a low Reynolds number;Applied Thermal Engineering;2024-02

5. Nonuniform height endwall fence optimization of a low-pressure turbine cascade;International Journal of Mechanical Sciences;2023-07

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