DEVIATION ANGLE DETERMINATION IN TRANSONIC AXIAL FLOW COMPRESSOR DESIGN

Cao Renjing; Tao Deping

Volume 9 Issue 3

Jul. 1994

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Article Navigation > Journal of Aerospace Power > 1994 > 9(3): 313-314,337

Cao Renjing, Tao Deping. DEVIATION ANGLE DETERMINATION IN TRANSONIC AXIAL FLOW COMPRESSOR DESIGN[J]. Journal of Aerospace Power, 1994, 9(3): 313-314,337.

Citation:

Cao Renjing, Tao Deping. DEVIATION ANGLE DETERMINATION IN TRANSONIC AXIAL FLOW COMPRESSOR DESIGN[J]. Journal of Aerospace Power, 1994, 9(3): 313-314,337.

Cao Renjing, Tao Deping. DEVIATION ANGLE DETERMINATION IN TRANSONIC AXIAL FLOW COMPRESSOR DESIGN[J]. Journal of Aerospace Power, 1994, 9(3): 313-314,337.

Citation:

Cao Renjing, Tao Deping. DEVIATION ANGLE DETERMINATION IN TRANSONIC AXIAL FLOW COMPRESSOR DESIGN[J]. Journal of Aerospace Power, 1994, 9(3): 313-314,337.

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DEVIATION ANGLE DETERMINATION IN TRANSONIC AXIAL FLOW COMPRESSOR DESIGN

4th Dept.,Beijing University of Aeronautics and Astronautics,Beijing 100083

Received Date: 1993-09-01
Rev Recd Date: 1993-11-01
Publish Date: 1994-07-28

Abstract

Abstract

The deviation angle determination in transonic axial compressor design is analyzed in detail.In addition,the aerodynamic and geometrical parameters acting on deviation angle distribution are discussed.A new deviation angle calculation formula is provided and applied to redesigning of an axial compressor stage.The results show that the aerodynamic and blade design is quite satisfactory.