Affiliation:
1. Ebara Research Company, Limited, Fujisawa-shi, Japan
2. Department of Mechanical Engineering, University College of London, London, United Kingdom
Abstract
In Part 1 of this paper, a mixed-flow pump impeller was designed by a fully three-dimensional inverse design method, aimed at suppressing the secondary flows on the blade suction surface. In this part, the internal flow fields of the impeller are investigated experimentally, using flow visualization and phase-locked measurements of the impeller exit flow, in order to validate the effects of secondary flow suppression. The flow fields are compared with those of a conventional impeller, and it is confirmed that the secondary flows on the blade suction surface are well suppressed and the uniformity of the exit flow fields is improved substantially, in both circumferential and spanwise directions. The effects of tip clearance and the number of blades for the inverse designed impeller are also investigated experimentally and numerically.
Reference7 articles.
1. Cumpsty, N. A., 1989, Compressor Aerodynamics, Longman Scientific & Technical, pp. 230–232.
2. Dawes, W. N., 1988, “Development of a 3D Navier–Stokes Solver for Application to All Types of Turbomachinery,” ASME Paper No. 88-GT-70.
3. Goto, A., 1988, “Phase-Locked Measurements of Three-Dimensional Periodic Flow from an Impeller Using a Two-Hole Pitot Probe,” Proc. 2nd International Symposium on Fluid Control and Measurements (FLUCOME ’88), Sheffield, United Kingdom, Sept. 5-9.
4. Goto
A.
, 1992a, “Study of Internal Flows in Mixed-Flow Pump Impellers With Various Tip Clearances using Three-Dimensional Viscous Flow Computations,” ASME JOURNAL OF TURBOMACHINERY, Vol. 114, pp. 373–382.
5. Goto
A.
, 1992b, “The Effect of Tip Leakage Flow on Part-Load Performance of a Mixed-Flow Pump Impeller,” ASME JOURNAL OF TURBOMACHINERY, Vol. 114, pp. 383–391.
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