Two-Dimensional Rotating Stall Analysis in a Wide Vaneless Diffuser

We report a numerical study on the vaneless diffuser core flow instability in centrifugal compressors. The analysis is performed for the purpose of better understanding of the rotating stall flow mechanism in radial vaneless diffusers. Since the analysis is restricted to the two-dimensional core flo...

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Main Authors: S. Ljevar, H. C. de Lange, A. A. van Steenhoven
Format: Article
Language:English
Published: Hindawi Limited 2006-01-01
Series:International Journal of Rotating Machinery
Online Access:http://dx.doi.org/10.1155/IJRM/2006/56420
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spelling doaj-50fe4403df3e42f5aadfa71bfcf394e42020-11-24T22:13:53ZengHindawi LimitedInternational Journal of Rotating Machinery1023-621X1542-30342006-01-01200610.1155/IJRM/2006/5642056420Two-Dimensional Rotating Stall Analysis in a Wide Vaneless DiffuserS. Ljevar0H. C. de Lange1A. A. van Steenhoven2Section of Energy Technology, Division Thermo Fluids Engineering, Department of Mechanical Engineering, Eindhoven University of Technology, Den Dolech 2, Eindhoven, MB 5600, The NetherlandsSection of Energy Technology, Division Thermo Fluids Engineering, Department of Mechanical Engineering, Eindhoven University of Technology, Den Dolech 2, Eindhoven, MB 5600, The NetherlandsSection of Energy Technology, Division Thermo Fluids Engineering, Department of Mechanical Engineering, Eindhoven University of Technology, Den Dolech 2, Eindhoven, MB 5600, The NetherlandsWe report a numerical study on the vaneless diffuser core flow instability in centrifugal compressors. The analysis is performed for the purpose of better understanding of the rotating stall flow mechanism in radial vaneless diffusers. Since the analysis is restricted to the two-dimensional core flow, the effect of the wall boundary layers is neglected. A commercial code with the standard incompressible viscous flow solver is applied to model the vaneless diffuser core flow in the plane parallel to the diffuser walls. At the diffuser inlet, rotating jet-wake velocity pattern is prescribed and at the diffuser outlet constant static pressure is assumed. Under these circumstances, two-dimensional rotating flow instability similar to rotating stall is found to exist. Performed parameter analysis reveals that this instability is strongly influenced by the diffuser geometry and the inlet and outlet flow conditions.http://dx.doi.org/10.1155/IJRM/2006/56420
collection DOAJ
language English
format Article
sources DOAJ
author S. Ljevar
H. C. de Lange
A. A. van Steenhoven
spellingShingle S. Ljevar
H. C. de Lange
A. A. van Steenhoven
Two-Dimensional Rotating Stall Analysis in a Wide Vaneless Diffuser
International Journal of Rotating Machinery
author_facet S. Ljevar
H. C. de Lange
A. A. van Steenhoven
author_sort S. Ljevar
title Two-Dimensional Rotating Stall Analysis in a Wide Vaneless Diffuser
title_short Two-Dimensional Rotating Stall Analysis in a Wide Vaneless Diffuser
title_full Two-Dimensional Rotating Stall Analysis in a Wide Vaneless Diffuser
title_fullStr Two-Dimensional Rotating Stall Analysis in a Wide Vaneless Diffuser
title_full_unstemmed Two-Dimensional Rotating Stall Analysis in a Wide Vaneless Diffuser
title_sort two-dimensional rotating stall analysis in a wide vaneless diffuser
publisher Hindawi Limited
series International Journal of Rotating Machinery
issn 1023-621X
1542-3034
publishDate 2006-01-01
description We report a numerical study on the vaneless diffuser core flow instability in centrifugal compressors. The analysis is performed for the purpose of better understanding of the rotating stall flow mechanism in radial vaneless diffusers. Since the analysis is restricted to the two-dimensional core flow, the effect of the wall boundary layers is neglected. A commercial code with the standard incompressible viscous flow solver is applied to model the vaneless diffuser core flow in the plane parallel to the diffuser walls. At the diffuser inlet, rotating jet-wake velocity pattern is prescribed and at the diffuser outlet constant static pressure is assumed. Under these circumstances, two-dimensional rotating flow instability similar to rotating stall is found to exist. Performed parameter analysis reveals that this instability is strongly influenced by the diffuser geometry and the inlet and outlet flow conditions.
url http://dx.doi.org/10.1155/IJRM/2006/56420
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AT hcdelange twodimensionalrotatingstallanalysisinawidevanelessdiffuser
AT aavansteenhoven twodimensionalrotatingstallanalysisinawidevanelessdiffuser
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