The evolution of the flow topologies of 3D separations in the stator passage of an axial compressor stage-Reference-Cited by-同舟云学术

The evolution of the flow topologies of 3D separations in the stator passage of an axial compressor stage

Published:2013-01 Issue: Volume:44 Page:301-311
ISSN:0894-1777
Container-title:Experimental Thermal and Fluid Science
language:en
Short-container-title:Experimental Thermal and Fluid Science

Author:

Yu Xianjun,Zhang Zhibo,Liu Baojie

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering

Reference27 articles.

1. Axial compressor stator aerodynamics;Joslyn;ASME Journal of Engineering for Gas Turbines and Power,1985

2. A comparison between the design point and near-stall performance of an axial compressor;McDougal;Journal of Turbomachinery,1990

3. V.-M. Lei, A Simple Criterion for Three-dimensional Flow Separation in Axial Compressors, PhD Thesis, Department of Aeronautics and Astronautics, MIT, 2006.

4. Experimental investigations of the three-dimensional flow in an annular compressor cascade;Schulz;Journal of Turbomachinery,1988

5. Three-dimensional separated flow field in the endwall region of an annular compressor cascade in the presence of rotor–stator interaction. Part I. Quasi-steady flow field and comparison with steady-state data;Schulz;Journal of Turbomachinery,1990

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