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Shape Optimization of High Power Centrifugal Compressor Using Multi-Objective Optimal Method
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다목적 최적화 기법을 이용한 고출력 원심압축기 형상 최적설계

논문 기본 정보

Type
Academic journal
Author
Hyun Su Kang (성균관대학교) Jeong Min Lee (성균관대학교) Youn Jea Kim (성균관대학교)
Journal
The Korean Society of Mechanical Engineers Transactions of the Korean Society of Mechanical Engineers - B Vol.39 No.5 KCI Accredited Journals SCOPUS
Published
2015.5
Pages
435 - 441 (7page)

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Shape Optimization of High Power Centrifugal Compressor Using Multi-Objective Optimal Method
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Abstract· Keywords

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In this study, a method for optimal design of impeller and diffuser blades in the centrifugal compressor using response surface method (RSM) and multi-objective genetic algorithm (MOGA) was evaluated. A numerical simulation was conducted using ANSYS CFX with various values of impeller and diffuser parameters, which consist of leading edge (LE) angle, trailing edge (TE) angle, and blade thickness. Each of the parameters was divided into three levels. A total of 45 design points were planned using central composite design (CCD), which is one of the design of experiment (DOE) techniques. Response surfaces that were generated on the basis of the results of DOE were used to determine the optimal shape of impeller and diffuser blade. The entire process of optimization was conducted using ANSYS Design Xplorer (DX). Through the optimization, isentropic efficiency and pressure recovery coefficient, which are the main performance parameters of the centrifugal compressor, were increased by 0.3 and 5, respectively.

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초록
Abstract
1. 서론
2. 수치해석
3. 최적설계
4. 결과 및 고찰
5. 결론
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UCI(KEPA) : I410-ECN-0101-2016-550-001469923