DocumentCode :
3596833
Title :
Numerical Simulation for Influence of Inducer Geometric Parameters on Performance
Author :
Li, Xiao-Jun ; Pan, Zhong-Yong ; Li, Shuai ; Kong, Fan-Yu
Author_Institution :
Res. Center of Fluid Machinery Eng. & Technol., Jiangsu Univ., Zhenjiang, China
Volume :
2
fYear :
2010
Firstpage :
94
Lastpage :
97
Abstract :
The influence of the geometric parameters on performance of inducer was deeply analyzed. A numerical simulation of the inducer was introduced by using software FLUENT. Reynolds Averaged Navier-Stokes equations was dispersed and solved with κ-ε turbulence model and the SIMPLE algorithm in double coordinate system. The numerical simulation predicted the distribution law of the pressure and velocity in inducer with different axial lengths and leading edge sharpened. The results show that there is an evident change of pressure and efficiency in the inducer as the axial length angle change, the best cascade solidity is between 2 ~ 3. The study also found that the leading edge sharpened can improve the performance of inducer, and moreover, the greater of the flow rate, the more obvious improvements in performance.
Keywords :
Navier-Stokes equations; flow simulation; geometry; mechanical engineering computing; numerical analysis; turbulence; κ-ε turbulence model; Reynolds averaged Navier-Stokes equations; SIMPLE algorithm; cascade solidity; double coordinate system; geometric parameters; inducer geometric parameters; inducer performance; numerical simulation; software FLUENT; Blades; Computational fluid dynamics; Design methodology; Equations; Impellers; Information analysis; Machinery; Numerical simulation; Performance analysis; Structural engineering; axial length; centrifugal pump; inducer; leading edge sharpened; numerical simulation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Information and Computing (ICIC), 2010 Third International Conference on
Print_ISBN :
978-1-4244-7081-5
Electronic_ISBN :
978-1-4244-7082-2
Type :
conf
DOI :
10.1109/ICIC.2010.117
Filename :
5514091
Link To Document :
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