Comparison of Computational Results Obtained From a Homogeneous Cavitation Model With Experimental Investigations of Three Inducers

Author:

Mejri Imene1,Bakir Farid1,Rey Robert1,Belamri Thabet2

Affiliation:

1. Laboratoire d’Energétique et de Mécanique de Fluides Interne (LEMFI), Site Paris UMR CNRS 7067, Ecole Nationale Supérieure d’Arts et Métiers (ENSAM), 151 Boulevard de l’Hopital 75013 Paris, France

2. ANSYS Canada, 554 Parkside Dr., Waterloo, Ontario, Canada

Abstract

The paper presents full 3D numerical simulations and experimental investigations of the cavitating flow through three axial inducers. These inducers are identified by the tip blade angle at the leading edge β1T=8, 10, and 13deg. The numerical and experimental investigations were carried out at the LEMFI laboratory (Laboratoire d’Energétique et de Mécanique de Fluides Interne) of the ENSAM-Paris center (Ecole Nationale Supérieure d’Arts et Métiers). A review of the cavitating regime modeling and the cavitation homogeneous model used for this paper’s calculations is first presented. The numerical model is based on a combination of the multiphase flow equations with a truncated version of the Rayleigh-Plesset model predicting the complicated growth and collapse processes of bubbles. The mass transfers due to cavitation are source/sink terms in continuity equations of the liquid and vapor phases. The cavitation model also features a solution methodology which implicitly couples the continuity and momentum equations together. The main results are presented for the inducers at a range of flow rates and cavitation numbers: (1) Experimental results concerning: (i) the overall performances: Pressure head coefficient and efficiency versus flow rates; (ii) critical cavitation number (5% and 15% of drop) versus the flow rate; (2) Numerical results concerning: (i) the overall performances; (ii) the numerically investigated water vapor volume fraction distributions and other CFD results, which enable us to explain the cavitating behavior for these inducers; (iii) the location and sizes of the blade cavity and backflow vortex. Finally, the comparisons between experimental and simulated results on the overall performances, cavity sizes and cavity location are discussed. A qualitative agreement between experimental and predicted results was found for two inducers for a range of flow rates. The head breakdown in the simulations started at a different cavitation coefficient than that in the experiment.

Publisher

ASME International

Subject

Mechanical Engineering

Reference40 articles.

1. Numerical and Experimental Investigations of the Cavitating Behavior of an Inducer;Bakir;Int. J. Rotating Mach.

2. Mejri, I., Bakir, F., Kouidri, S., and Rey, R., 2003, “Hub Shape Effects under Cavitation on the Inducers Performance,” Fifth International Symposium on Cavitation (CAV 2003). OS-6-001, Osaka, Japan, November 1–4, 2003.

3. Bakir, F., Kouidri, S., Noguera, R., and Rey, R., 1998, “Design and Analysis of Axial Inducers Performance,” ASME Fluid Machinery Forum, Washington, D.C., paper FEDSM98 - 5118.

4. Noguera, R., Rey, R., Massouh, F., Bakir, F., and Kouidri, S., 1993, “Design and Analysis of Axial Pumps,” ASME Fluids Engineering, Second Pumping Machinery Symposium, pp. 95–111, Washington, USA.

5. Influence of Peripheral Blade Angle on the Performance and the Stability of Axial Inducers;Mejri;IMECH E Journal of Power and Energy, A04404

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