Experimental investigation on the momentumless wake using trailing edge blowing

Author:

Wu Y1,Zhu X1,Du Z1

Affiliation:

1. School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai, People's Republic of China

Abstract

A developed plate stator model with and without trailing edge blowing (TEB) is studied using experimental methods. Wake characteristics of flow over the stator in the three-dimensional wake regimes are studied using hot-wire anemometry (HWA) and particle image velocimetry (PIV) techniques. First, the mean velocity profiles have been measured in the wake of the stator using HWA. Four wake characteristics have been obtained through momentum thickness judgments: pure wake, weak wake, momentumless wake, and jet. These velocity profiles show some differences in momentum deficit for the four cases. Then, the velocity spectra of the pure wake and momentumless wake obtained through the HWA measurements showed that TEB can eliminate the shedding vortex of the stator. Characteristic length scales based on the wake turbulent intensity profiles showed that the momentumless wake can reduce the wake width and depth. PIV measurement is carried out to measure the flow field of the four wakes. Finally, the application of TEB approaching momentumless wake status is used on an industrial ventilation low-pressure axial fan to assess noise reduction. The results show that TEB can make the outlet of the stator uniform, reduce velocity fluctuation, destroy the vorticity structure downstream of the stator, and reduce interaction noise level of the stator and rotor.

Publisher

SAGE Publications

Subject

Mechanical Engineering

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Minimization of time-averaged and unsteady aerodynamic forces on a thick flat plate using synthetic jets;Journal of Fluids and Structures;2015-04

2. An analytical investigation of stator lean on rotor–stator interaction noise;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2014-03-17

3. Investigation about Rotor-stator Interaction with an Adjustable Leaned Vane Blade;International Journal of Turbo & Jet-Engines;2014-01-01

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