Abstract
A CFD code with 2-D cascade model was developed to predict the cavitation behavior around the impeller blades of impeller in a centrifugal pump. The governing equations are the two-phase Reynolds Averaged Navier-Stokes equations in a homogeneous form in which both liquid and vapor phases are treated as incompressible fluid. To close the model, a standard k-ɛ turbulence model is introduced. And the mass transfer rates between liquid and vapor phases are implemented as well. The validations are carried out by comparing with reference data in impeller of a centrifugal pump impeller. The cavitation characteristics of current centrifugal pumps is tested at an ondesign point (V=8 m/s) and two off-design points (V=20 m/s and V=30 m/s), respectively. The criteria of cavitation and flow instability around blades are presented. The results show that the current centrifugal pump can safely operate without cavitation at on-design point. Also, the simulation shows cavitation develops inhomogeneously among the blades at off-design points. Moreover, the effects of additional blades in the impeller are studied as well. From the numerical results, it is expected that a half-length blade is the optimum configuration as additional blades in cavitation point of view.
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This paper was recommended for publication in revised form by Associate Editor Won-Gu Joo
Quangnha Thai received his B.S. in Aeronautical Engineering from Ho Chi Minh City University of Technology (HCMUT, Vietnam) and Ecole nationale superieure de mecanique et d’aerotechnique (ENSMA, France) in 2007. He is pursuing his M.S. in Aerospace Information Engineering from Konkuk University in Seoul, Korea. His research interests are in the area of computational fluid dynamics of two-phase flow and flow instability of rocket liquids.
Changjin Lee received his B.S. and M.S. in Aeronautical Engineering from Seoul National University in 1983 and 1985. He then went on to receive his Ph.D. from University of Illinois at Urbana-Champaign in 1992. Dr. Lee is currently a Professor at the department of Aerospace Engineering at Konkuk University in Seoul, Korea. His research interests are in the area of combustion instabilities of hybrid, liquid rocket and jet propulsions.
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Thai, Q., Lee, C. The cavitation behavior with short length blades in centrifugal pump. J Mech Sci Technol 24, 2007–2016 (2010). https://doi.org/10.1007/s12206-010-0705-9
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DOI: https://doi.org/10.1007/s12206-010-0705-9