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Peculiarities of Aerodynamic Design of High-Pressure Stages of Multistage Axial Compressors

Authors: Arkhipov D.V. Published: 07.10.2013
Published in issue: #3(80)/2010  

DOI:

 
Category: Power-generating and Transport Machine Building  
Keywords: axial compressor, theoretical work, reduced speed, diffuser factor, computational fluid dynamics

Effects of the reduced circular speed within the values range of λυ = 0.5 ... 1.25, the theoretical work coefficient Ηm = 0.2 ... 0.6 as well as the grid's density on the axial compressor's pressure are considered. The verification of the ANSYS CFX 11.0 program package is given which demonstrates the application of the three-dimensional computation method for designing stages of the axial compressor.