COMPUTER-AIDED EXPERIMENTAL INVESTIGATION OF AXIAL-FLOW COMPRESSORS

Zhu Nianguo; Chen Maozhang

Volume 2 Issue 2

Apr. 1987

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Zhu Nianguo, Chen Maozhang. COMPUTER-AIDED EXPERIMENTAL INVESTIGATION OF AXIAL-FLOW COMPRESSORS[J]. Journal of Aerospace Power, 1987, 2(2): 165-166,190.

Citation:

Zhu Nianguo, Chen Maozhang. COMPUTER-AIDED EXPERIMENTAL INVESTIGATION OF AXIAL-FLOW COMPRESSORS[J]. Journal of Aerospace Power, 1987, 2(2): 165-166,190.

Zhu Nianguo, Chen Maozhang. COMPUTER-AIDED EXPERIMENTAL INVESTIGATION OF AXIAL-FLOW COMPRESSORS[J]. Journal of Aerospace Power, 1987, 2(2): 165-166,190.

Citation:

Zhu Nianguo, Chen Maozhang. COMPUTER-AIDED EXPERIMENTAL INVESTIGATION OF AXIAL-FLOW COMPRESSORS[J]. Journal of Aerospace Power, 1987, 2(2): 165-166,190.

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COMPUTER-AIDED EXPERIMENTAL INVESTIGATION OF AXIAL-FLOW COMPRESSORS

Beijing Institute of Aeronautics and Astronautics

Received Date: 1986-06-01
Publish Date: 1987-04-28

Abstract

Abstract

An approach has been developed to evaluate some important aerodynamic parameterssuch as air-flow angle, blockage factor and loss coefficient, at immeasurablesurfaces. It can be used for two cases of measurement of multi-stage, axial-flow compressors. In order to testify this approach, several examples have been calculated and the results show that this approach provides reliable data for further performance improvement.