Effects of probe support on the stall characteristics of a low-speed axial compressor

Author:

Ma Hongwei,Li Shaohui,Wei Wei

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference12 articles.

1. Dudziniski T J, Krause L N. Effect of Inlet Geometry on Flow Angle Characteristics of Miniature Total Pressure Tubes. NACA TN D-6406, 1971.

2. Simon Coldrick, Paul Ivey, Roger Wells. Considerations for Using 3-D Pneumatic Probes in High-Speed Axial Compressors. Journal of Turbomachinery 2003, 125: 149–154

3. Lepicovsky J. Effects of a Rotating Aerodynamic Probe on the Flow Field of a Compressor Rotor. NASA/CR-2008-215215, 2008.

4. XIANG Honghui, REN Minlin, MA Hongwei, et al. Experimental and numerical investigation of airfoil probe influences on the performance of compressor cascade. Gas Turbine Experiment and Research 2010, 23(4): 10–16 [in Chinese]

5. XIANG Honghui, REN Minlin, MA Hongwei, et al. Effect of airfoil probes on the experimental results of axial flow compressor performance. Gas Turbine Experiment and Research 2008, 24(4): 28–33 [in Chinese]

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