This paper presents an experimental investigation of the effects of air injection on the rotating stall instability in a low speed axial compressor. Two experiments concerning air injection were tried. The first experiment used a continuous forcing perpendicular to the flow in the same or opposite direction of the tip velocity. The results show a dramatic difference between the two directions, with opposite direction forcing causing a significant increase in performance, and same direction forcing causing a significant decrease in performance. This result contradicts the Emmons stall propagation model. The second experiment investigated the differences with respect to different frequencies of air injection, with the injector pointed at the fan, parallel to the flow. We found that the change in the compressor characteristic in the unstalled region was highly dependent upon the forcing frequency with the maximum change occurring near the frequency of stall.
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ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition
June 5–8, 1995
Houston, Texas, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7878-1
PROCEEDINGS PAPER
Experimental Evaluation of Air Injection for Actuation of Rotating Stall in a Low Speed, Axial Fan
Richard M. Murray
Richard M. Murray
California Institute of Technology, Pasadena, CA
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Asif Khalak
Cornell University, Ithaca, NY
Richard M. Murray
California Institute of Technology, Pasadena, CA
Paper No:
95-GT-120, V001T01A027; 8 pages
Published Online:
February 16, 2015
Citation
Khalak, A, & Murray, RM. "Experimental Evaluation of Air Injection for Actuation of Rotating Stall in a Low Speed, Axial Fan." Proceedings of the ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition. Volume 1: Turbomachinery. Houston, Texas, USA. June 5–8, 1995. V001T01A027. ASME. https://doi.org/10.1115/95-GT-120
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