Optimization Strategy for an Axial-Flow Compressor Using a Region-Segmentation Combining Surrogate Model-Reference-Cited by-同舟云学术

Optimization Strategy for an Axial-Flow Compressor Using a Region-Segmentation Combining Surrogate Model

Published:2018-09 Issue:5 Volume:31 Page:04018076
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Lu Hanan¹,Li Qiushi²,Pan Tianyu³

Affiliation:

1. Research Scientist, National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang Univ., No. 37 Xueyuan Rd., Haidian District, Beijing 100191, China.

2. Professor, National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Collaborative Innovation Center of Advanced Aero-Engine, Beihang Univ., No. 37 Xueyuan Rd., Haidian District, Beijing 100191, China.

3. Research Scientist, National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Collaborative Innovation Center of Advanced Aero-Engine, Beihang Univ., No. 37 Xueyuan Rd., Haidian District, Beijing 100191, China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000907

Reference27 articles.

1. Sensitivity of Multistage Compressor Performance to Inlet Boundary Conditions

2. Wind Turbine Design Optimization Under Environmental Uncertainty

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

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

5. The exploitation of three-dimensional flow in turbomachinery design

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