Predicted and measured surface velocity and pressure distributions in the internal flow channels of a centrifugal fan impeller are presented for volume flow rates between 80 and 125 percent of design flow rate. Predictions are based on a fully three-dimensional, finite element analysis of the inviscid, incompressible blade channel flow. Additional predictions using a conventional quasi-three-dimensional analysis are presented for comparison. Experimental results were developed using extensive blade and sidewall surface pressure taps installed in a scale model of an airfoil-bladed centrifugal fan impeller designed for heavy industrial and power generation applications. The results illustrate the ability of both flow analyses to predict the dominant features of the impeller flow field, including peak blade surface velocities and adverse gradients at flows far from the design point. In addition, the experimental results provide valuable insight into the limiting channel diffusion values for typical centrifugal cascade performance, and the influence of viscous effects as seen in deviations from the ideal flow predictions.
Skip Nav Destination
Article navigation
October 1984
Research Papers
Flow in a Centrifugal Fan Impeller at Off-Design Conditions
T. Wright,
T. Wright
Westinghouse Fluid Systems Laboratory, West Lafayette, Ind. 47906
Search for other works by this author on:
K. T. S. Tzou,
K. T. S. Tzou
Westinghouse R&D Center, Pittsburgh, Pa.
Search for other works by this author on:
S. Madhavan
S. Madhavan
Westinghouse Sturtevant Division, Hyde Park, Mass.
Search for other works by this author on:
T. Wright
Westinghouse Fluid Systems Laboratory, West Lafayette, Ind. 47906
K. T. S. Tzou
Westinghouse R&D Center, Pittsburgh, Pa.
S. Madhavan
Westinghouse Sturtevant Division, Hyde Park, Mass.
J. Eng. Gas Turbines Power. Oct 1984, 106(4): 913-919 (7 pages)
Published Online: October 1, 1984
Article history
Received:
January 12, 1984
Online:
October 15, 2009
Citation
Wright, T., Tzou, K. T. S., and Madhavan, S. (October 1, 1984). "Flow in a Centrifugal Fan Impeller at Off-Design Conditions." ASME. J. Eng. Gas Turbines Power. October 1984; 106(4): 913–919. https://doi.org/10.1115/1.3239657
Download citation file:
Get Email Alerts
Cited By
Microtomography of Soil and Soot Deposits: Analysis of Three-Dimensional Structures and Surface Morphology
J. Eng. Gas Turbines Power
Modeling and Cycle Parameter Matching of a High-Speed Variable Cycle Turbofan-Ramjet Engine
J. Eng. Gas Turbines Power
Real Time Precursor Calculation for the Early Detection of Combustion Instabilities
J. Eng. Gas Turbines Power
Related Articles
Analysis and Validation of a Unified Slip Factor Model for Impellers at Design and Off-Design Conditions
J. Turbomach (October,2011)
Influence of Loading Distribution on the Performance of Transonic High Pressure Turbine Blades
J. Turbomach (April,2004)
Aerodynamic Design and Performance of Aspirated Airfoils
J. Turbomach (January,2003)
Active Control of Flow Separation in a Radial Blower
J. Fluids Eng (May,2010)
Related Proceedings Papers
Related Chapters
Boundary Layer Analysis
Centrifugal Compressors: A Strategy for Aerodynamic Design and Analysis
Antilock-Braking System Using Fuzzy Logic
International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3
Aerodynamic Performance Analysis
Axial-Flow Compressors