Analysis and Improvement of a Two-Stage Centrifugal Compressor Used in an MW-Level Gas Turbine

The performance of a low/high-pressure-stage centrifugal compressor in a land-use MW-level gas turbine with a pressure ratio of approximately 11 is analyzed and optimized with a 1D aerodynamic design and modeling optimization system. 1D optimization results indicate that the diameter ratio of the lo...

Full description

Bibliographic Details
Main Authors: Wei Zhu, Xiao-Dong Ren, Xue-Song Li, Chun-Wei Gu
Format: Article
Language:English
Published: MDPI AG 2018-08-01
Series:Applied Sciences
Subjects:
Online Access:http://www.mdpi.com/2076-3417/8/8/1347