The phenomena of vortex formation in relative flow field of a radial flow centrifugal pump, running at zero and part loads of the pump discharge, has been investigated. The flow field is described by two dimensional Poisson's equation, which has been solved numerically, in difference form, by relaxation technique. A physical model for the vortex formation and shedding mechanisms, at part loads, has been introduced. The effect of vortex shedding, from the impeller, on the pressure fluctuation at the pump exit has been also discussed. Experimental investigation has shown a satisfactory agraement between the measured and the theoretically predicted pressure fluctuations at part flow rates. At high flow rates, the viscosity effect on the vortex simulation model, has to be considered.
SALEH, I., & LOTFY, A. (1991). VORTEX SIMULATION IN RADIAL FLOW IMPELLERS OF CENTRIFUGAL PUMPS AT PART LOADS. International Conference on Aerospace Sciences and Aviation Technology, 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO), 155-163. doi: 10.21608/asat.1991.25674
MLA
I. SALEH; A. H. LOTFY. "VORTEX SIMULATION IN RADIAL FLOW IMPELLERS OF CENTRIFUGAL PUMPS AT PART LOADS", International Conference on Aerospace Sciences and Aviation Technology, 4, ASAT CONFLENCE 14-16 May 1991 , CAIRO, 1991, 155-163. doi: 10.21608/asat.1991.25674
HARVARD
SALEH, I., LOTFY, A. (1991). 'VORTEX SIMULATION IN RADIAL FLOW IMPELLERS OF CENTRIFUGAL PUMPS AT PART LOADS', International Conference on Aerospace Sciences and Aviation Technology, 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO), pp. 155-163. doi: 10.21608/asat.1991.25674
VANCOUVER
SALEH, I., LOTFY, A. VORTEX SIMULATION IN RADIAL FLOW IMPELLERS OF CENTRIFUGAL PUMPS AT PART LOADS. International Conference on Aerospace Sciences and Aviation Technology, 1991; 4(ASAT CONFLENCE 14-16 May 1991 , CAIRO): 155-163. doi: 10.21608/asat.1991.25674
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