Optimization of a transonic axial-flow compressor under inlet total pressure distortion to enhance aerodynamic performance-Reference-Cited by-同舟云学术

Optimization of a transonic axial-flow compressor under inlet total pressure distortion to enhance aerodynamic performance

Published:2020-01-01 Issue:1 Volume:14 Page:1002-1022
ISSN:1994-2060
Container-title:Engineering Applications of Computational Fluid Mechanics
language:en
Short-container-title:Engineering Applications of Computational Fluid Mechanics

Author:

Da Li¹,Hanan Lu¹,Zhe Yang¹,Tianyu Pan¹,Hai Du²,Qiushi Li¹²

Affiliation:

1. National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University, Beijing, People’s Republic of China

2. Key Laboratory of Fluid and Power Machinery, Xihua University, Chengdu, People’s Republic of China

Funder

National Natural Science Foundation of China

China Postdoctoral Science Foundation

Xihua University

Publisher

Informa UK Limited

Subject

Modelling and Simulation,General Computer Science

Link

https://www.tandfonline.com/doi/pdf/10.1080/19942060.2020.1792348

Reference39 articles.

1. Computational intelligence approach for modeling hydrogen production: a review

2. Aerodynamics of swept and leaned transonic compressor-rotors

3. Shock/Boundary-Layer/Tip-Clearance Interaction in a Transonic Rotor Blade

4. Optimization of Wind Turbine Blade Airfoils Using a Multi-Objective Genetic Algorithm

5. Shape optimization of airfoils in transonic flow using a multi-objective genetic algorithm

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