CFD Validation and Analysis of a Single-Stage Axial Compressor

Author:

Xiang Jun Ting1,Schlüter Jӧrg Uwe1,Duan Fei1

Affiliation:

1. Nanyang Technological University

Abstract

The knowledge about changes of flow field properties during axial compressor operationat high and relatively low speed is limited. This work provides a numerical approach to addressthese problems. Validations about the numerical scheme and the test of compressor performance at various operating speeds are conducted. The results show that computational fluid dynamics (CFD)is capable in predicting the compressor performance. Flow property changes during the compressoroperation are discussed and explanations are proposed. This work reinforces the understanding of compressor operation and provides valid results for future reference.

Publisher

Trans Tech Publications, Ltd.

Reference14 articles.

1. Information on http: /www. pw. utc. com.

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3. Reid, L. and R.D. Moore, Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratio of 1. 19 and 1. 26, respectively, and with design pressure ratio of 1. 82. NASA Technical Paper, 1978. 1338.

4. Day, I.J., Axial compressor performance during surge. Journal of Propulsion and Power, 1994. 10(3): pp.329-336.

5. Spakovszky, Z.S., Active control of rotating stall in a transonic compressor stage with inlet distortion. (1999).

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