On the performance of a radial pump impeller by varying the outlet blade angle
The systematic research on the influence of the various design aspects of a centrifugal pump in its performance in the whole range of the flow rates requires numerical predictions and experiment. The present ongoing research is concerned with the influence of the outlet blade angle in the performance of a laboratory centrifugal pump fitted in the pump test rig in the Fluid Mechanics Laboratory of the University of Patras.
The design and off-design performance characteristic curves, the local and global variables of the flow field and the resulted non-uniform circumferential pressure field are numerically predicted for three shrouded radial impellers with different outlet blade angle. The computational fluid dynamics analysis is carried out with the commercial software package Fluent which has been widely used in the field of turbomachinery.
The volute of the laboratory centrifugal pump is of rectangular section with rounded corners and its diffuser extends in the radial direction. Three shrouded impellers of constant width (b=20mm) with six untwisted blades backward facing have been designed according to Pfleiderer method. The blade length in the three impellers is almost equal. All impellers have the same diameters in suction and pressure side as well as the same blade’s leading edge angle (β1=14 deg) and they vary in the blade’s trailing edge angle which is β2=20, 30 and 50 deg, respectively. The diameters of the impellers at the suction and pressure side are D1=150mm and D2=280mm, respectively.
The incompressible flow through the rotating impeller is solved in a moving frame of reference with constant rotational speed equal the rotational speed of the impeller. The flow through the stationary parts of the pump is solved in an inertial reference frame. The turbulence of the flow is modeled with standard k-ε model that is rated as the most used model that combines simplicity, robustness and reasonable accuracy.


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