Numerical investigation of base-setting of stator’s stagger angles for a 15-stage axial-flow compressor

Author:

Chang Hao,Zhao Weiguang,Jin Donghai,Peng Zeyan,Gui Xingmin

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference10 articles.

1. Ronald D F. Fundamentals of jet propulsion with applications. Cambridge University Press, Cambridge, UK, (2005).

2. R. R. Woollett, Aerodynamic Performance of a Fan Stage Utilizing Variable Inlet Guide Vanes for Thrust Modulation, AIAA/SAE/ASME 19th Joint Propulsion Conference, AIAA-83-1162, Seattle, USA, (1983).

3. Celis, Cesar, et al. Modeling of Variable Inlet Guide Vanes Affects on a One Shaft Industrial Gas Turbine Used in a Combined Cycle Application. ASME paper GT2008-50076, Berlin, Germany, (2008).

4. Abdollah Shadaram, et al. Optimization of Variable Stator’s Angle for Off Design Compression Systems Using Streamline Curvature Method, ASME paper GT2009-59772, Orlando, USA, (2009).

5. Sun J, Elder R L. Numerical optimization of a stator vane setting in multistage axial-flow compressors. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 212(4): 247–259, (1998).

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