Blade Number Selection for a Splittered Mixed-Flow Compressor Impeller Using Improved Loss Model
Author:
Affiliation:
1. School of Energy and Power Engineering , Beihang University , Beijing 100191 , China
2. Beijing Research Institute of Precise Mechatronics and Controls , Beijing 100076 , China
Abstract
Publisher
Walter de Gruyter GmbH
Subject
Aerospace Engineering
Link
https://www.degruyter.com/document/doi/10.1515/tjj-2020-0008/pdf
Reference34 articles.
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3. Aungier RH. Mean streamline aerodynamic performance analysis of centrifugal compressors. J Turbomach. 1995;117:360–6.
4. Oh HW, Yoon ES, Chung MK. An optimum set of loss models for performance prediction of centrifugal compressors. Proc Inst Mech Eng Part A: J Power Energy. 1997;211:331–8.
5. Li PY, Gu CW, Song Y. A new optimization method for centrifugal compressors based on 1D calculations and analyses. Energies. 2015;8:4317–34.
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