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Comparative study of subsynchronous rotating flow patterns in centrifugal compressors with vaneless diffusersA comparative experimental investigation of the unstable operating modes of a centrifugal compressor was made. Impeller and/or diffuser rotating stall was observed, depending on the flow conditions. The measured relative rotational speed of this perturbation is cross checked with other experimental data and it is shown that the rotational speed is strongly dependent on the type of rotating stall. The diffuser absolute inlet flow angle at the onset of diffuser rotating stall agrees well with the value predicted by an existing stability criterion.
Document ID
19830007381
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Frigne, P.
(State Univ. of Gent)
Vandenbraembussche, R.
(Von Karman Inst. for Fluid Dynamics)
Date Acquired
August 11, 2013
Publication Date
December 1, 1982
Publication Information
Publication: NASA. Lewis Research Center Rotordyn. Instability Probl. in High-Performance Turbomachinery
Subject Category
Mechanical Engineering
Accession Number
83N15652
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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