Aerodynamic performance improvement of a transonic compressor rotor with a small plate near the leading edge

Author:

Wang Naian,Luo Dan,Wu Yujing,Zhou Yangwei,Guo Dange,Huang Diangui

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Reference33 articles.

1. H. Zhang, Structural Analysis of Separated Flow and Vortex Motion, National Defense Industry Press, Beijing (2005).

2. Y. Li, L. V. Biao and D. Ye, Study on three-dimensional separated flow characteristics in annular compressor cascade at high angle of attack, Journal of Engineering Thermophysics, 913(3) (1992) 254–260.

3. Y. Lu, Unsteady Flow Theory of Turbomachinery, Beijing University of Aeronautics and Astronautics Press, Beijing (1990).

4. R. P. Dring, H. D. Joslyn and L. W. Hardin, Investigation of axial compressor rotor aerodynamics, Journal of Engineering for Gas Turbines and Power, 104(1) (1982) 84–96.

5. N. Gourdain, F. Wlassow and X. Ottavy, Effect of tip clearance dimensions and control of unsteady flows in a multi-stage high-pressure compressor, Journal of Turbomachinery, 134(5) (2012) 597–626.

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