Investigation of the Effects of Airfoil-probes on the Aerodynamic Performance of an Axial Compressor-Reference-Cited by-同舟云学术

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Investigation of the Effects of Airfoil-probes on the Aerodynamic Performance of an Axial Compressor

Published:2012-08 Issue:4 Volume:25 Page:517-523
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

HE Xiang,MA Hongwei,REN Minglin,XIANG Honghui

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference13 articles.

1. Dudzinski T J. Effect of inlet geometry on flow-angle characteristics of miniature total pressure tubes. NASA TN-D-6404, 1971.

2. Comparison of transonic flow calculations with experimental data;Lehmann,1982

3. Barankiewicz W S, Hathaway M D. Effects of stator indexing on performance in a low speed multistage axial compressor. NASA TM-113113, 1997.

4. Experimental investigation of parameter measurements in an axial-flow multistage compressor;Xing;Journal of Aerospace Power,2004

5. Experimental investigation on an axial-flow multistage compressor;Cui;Gas Turbine Experiment and Research,2005

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