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Effects of circumferential configuration concerning splitter blade on the aerodynamic performance in

本站小编 哈尔滨工业大学/2019-10-23

Effects of circumferential configuration concerning splitter blade on the aerodynamic performance in a transonic axial fan

Xue Liang, HuanWanJin

Propulsion Theory and Technic Academy, Harbin Institute of Technology, Harbin 150001, China



Abstract:

For a certain type of transonic axial fan, the flow field of a fan rotor with splitter blade was computed by numerical simulation, and the shape of the rotor was modified. The effects of different circumferential distributions concerning the splitter cascades upon the aerodynamic performance were investigated. The studies show that the optimum splitter cascade is not very close to the suction side of main blade. The load between the main blade and the splitter blade can be soundly distributed in terms of the adjustment of circumferential position of the splitter blade. The best aerodynamic performance can be successfully obtained according to the optimum shape of the expanding fluid channel reasonably formed by the splitter blade and the main blade.

Key words:  transonic axial fan  splitter blade  shock wave  flow loss  compressor

DOI:10.11916/j.issn.1005-9113.2010.01.014

Clc Number:TH453

Fund:


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