Unsteady Flow Field Investigations at Near Stall for a Transonic Compressor Rotor by Proper Orthogonal Decomposition

Author:

Liu Zhenxiong1

Affiliation:

1. Shanghai Civil Aviation College, China

Publisher

ACM

Reference19 articles.

1. Inoue , M. and Kuroumaru , M. Detection of a Rotating Stall Precursor in Isolated Axial Flow Compressor Rotors.ASME J.Turbomach 199 1; 113(2), paper no.281-289. Inoue, M. and Kuroumaru, M.Detection of a Rotating Stall Precursor in Isolated Axial Flow Compressor Rotors.ASME J.Turbomach 1991; 113(2), paper no.281-289.

2. Furukawa M and Inoue M. The Role of Tip Leakage Vortex Breakdown in Compressor Rotor Aerodynamics. ASME J.Turbomach 199 9; 121(3), paper no.469-480. Furukawa M and Inoue M.The Role of Tip Leakage Vortex Breakdown in Compressor Rotor Aerodynamics. ASME J.Turbomach 1999; 121(3), paper no.469-480.

3. Vo H D and Tan C S.Criteria for Spike Initiated Rotating Stall[J].ASME Journal of Turbomachinery 2005:130(1). Vo H D and Tan C S.Criteria for Spike Initiated Rotating Stall[J].ASME Journal of Turbomachinery 2005:130(1).

4. Bergner J.and Kinzel M.Short Length-Scale Rotating Inception in a Transonic Axial Compressor Experimental Investigation.ASME paper no. GT2006-90209. Bergner J.and Kinzel M.Short Length-Scale Rotating Inception in a Transonic Axial Compressor Experimental Investigation.ASME paper no. GT2006-90209.

5. Hah C.and Bergner J.Short Length Scale Rotating Stall Inception in a Transonic Axial Compressor Criteria and Mechanisms. ASME paper no. GT2006-90045. Hah C.and Bergner J.Short Length Scale Rotating Stall Inception in a Transonic Axial Compressor Criteria and Mechanisms. ASME paper no. GT2006-90045.

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