Aerodynamic design and strength check of a two-stage dual-rotor opposed centrifugal compressor

<b>[Objectives]</b> To accomplish the design of a two-stage dual-rotor opposed centrifugal compressor for a small gas turbine,<b>[Methods]</b> the compressor is subject to aerodynamic design and three-dimensional flow field check by using the software Concepts NREC and the Nu...

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Bibliographic Details
Main Authors: Geng Shaojuan, Ni Ming, Ding Linchao, Wang Wentao, Zhang Xiaoyu
Format: Article
Language:English
Published: Editorial Office of Chinese Journal of Ship Research 2019-08-01
Series:Zhongguo Jianchuan Yanjiu
Subjects:
Online Access:http://www.ship-research.com/EN/Y2019/V14/I4/111