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Active control of vaneless diffuser rotating stallExperiments were carried out to study the feasibility of active stabilization of vaneless diffuser rotating stalls. Pressure fluctuation at the diffuser inlet was monitored and used to control the rotating stall. AC control flow, which is produced by a load speaker, was introduced into the diffuser at the inlet. It is shown that the rotating stall can be suppressed when the phase of the control flow has a certain relation with the phase of the rotating stall. By considering the energy flux due to the AC control flow, it is shown that the rotating stall is suppressed when the control flow has the phase such that the energy is subtracted out from the diffuser flow. Discussions are made on the relations between the energy flux and the amplitude of the pressure fluctuation due to the rotating stalls.
Document ID
19940029672
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yoshida, Yoshiki
(Osaka Univ. Toyonaka, Japan)
Tsujimoto, Yoshinobu
(Osaka Univ. Toyonaka, Japan)
Tateishi, Tomohiro
(Osaka Univ. Toyonaka, Japan)
Tsurusaki, Hiromu
(Osaka Univ. Toyonaka, Japan)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Publication Information
Publication: NASA. Lewis Research Center, Rotordynamic Instability Problems in High-Performance Turbomachinery, 1993
Subject Category
Mechanical Engineering
Accession Number
94N34178
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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