Computational fluid dynamics (CFD) is nowadays extensively used for turbomachinery design and performance prediction. Nevertheless, compressors numerical simulations still fail in correctly predicting the stall inception and the poststall behavior. Several authors address such a lack of accuracy to the incomplete definition of the boundary conditions and of the turbulence parameters at the inlet of the numerical domain. The aim of the present paper is to contribute to the development of compressors CFD by providing a complete set of input data for numerical simulations. A complete characterization has been carried out for a state-of-art 1.5 stage highly loaded low-pressure compressor for which previous CFD analyses have failed to predict its behavior. The experimental campaign has been carried out in the R4 facility at the Von Karman Institute for Fluid Dynamics (VKI). The test item has been tested in different operative conditions for two different speed lines (90% and 96% of the design speed) and for two different Reynolds numbers. Stable and unstable operative conditions have been investigated along with the stalling behavior, its inception, and the stall-cell flow field. Discrete hot-wire traverses have been performed in order to characterize the spanwise velocity field and the turbulence characteristics.
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Complete Characterization of a Highly Loaded Low Pressure Compressor at Different Reynolds Numbers for Computational Fluid Dynamics Simulations
Ruzbeh Hadavandi,
Ruzbeh Hadavandi
Jacques Chauvin Laboratory,
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
Rhode-St-Genèse B-1640, Belgium
e-mail: rhadavandi@hotmail.com
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
Rhode-St-Genèse B-1640, Belgium
e-mail: rhadavandi@hotmail.com
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Fabrizio Fontaneto,
Fabrizio Fontaneto
Jacques Chauvin Laboratory,
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
Rhode-St-Genèse B-1640, Belgium
e-mail: fontaneto@vki.ac.be
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
Rhode-St-Genèse B-1640, Belgium
e-mail: fontaneto@vki.ac.be
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Julien Desset
Julien Desset
Jacques Chauvin Laboratory,
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
B-1640 Rhode-St-Genèse, Belgium
e-mail: desset@vki.ac.be
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
B-1640 Rhode-St-Genèse, Belgium
e-mail: desset@vki.ac.be
Search for other works by this author on:
Ruzbeh Hadavandi
Jacques Chauvin Laboratory,
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
Rhode-St-Genèse B-1640, Belgium
e-mail: rhadavandi@hotmail.com
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
Rhode-St-Genèse B-1640, Belgium
e-mail: rhadavandi@hotmail.com
Fabrizio Fontaneto
Jacques Chauvin Laboratory,
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
Rhode-St-Genèse B-1640, Belgium
e-mail: fontaneto@vki.ac.be
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
Rhode-St-Genèse B-1640, Belgium
e-mail: fontaneto@vki.ac.be
Julien Desset
Jacques Chauvin Laboratory,
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
B-1640 Rhode-St-Genèse, Belgium
e-mail: desset@vki.ac.be
Turbomachinery and Propulsion Department,
Von Karman Institute for Fluid Dynamics,
Chaussée de Waterloo 72,
B-1640 Rhode-St-Genèse, Belgium
e-mail: desset@vki.ac.be
1Corresponding author.
Contributed by the Heat Transfer Division of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received February 7, 2018; final manuscript received February 26, 2018; published online May 2, 2018. Editor: Kenneth Hall.
J. Turbomach. May 2018, 140(6): 061008 (9 pages)
Published Online: May 2, 2018
Article history
Received:
February 7, 2018
Revised:
February 26, 2018
Citation
Hadavandi, R., Fontaneto, F., and Desset, J. (May 2, 2018). "Complete Characterization of a Highly Loaded Low Pressure Compressor at Different Reynolds Numbers for Computational Fluid Dynamics Simulations." ASME. J. Turbomach. May 2018; 140(6): 061008. https://doi.org/10.1115/1.4039727
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