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Research Article | Publishing Language: Chinese | Open Access

The influence of splitter on the flow dynamics in a continuous-discrete pulsing jet fluidic oscillator

Institute of Turbomachinery, School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai 200240, China
Low Speed Aerodynamics Institute of China Aerodynamics Research and Development Center, Mianyang 621000, China
Aero Engine Academy of China, Aero Engine Corporation of China, Beijing 101304, China
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Abstract

This paper studies the internal flow dynamics of a continuous-discrete pulsing jet fluidic oscillator and the influence of splitter on its outlet peak velocity and oscillating frequency. For that purpose, two-dimensional unsteady numerical simulations were conducted, covering five different inlet mass flowrates m˙ and three oscillator models (two continuous-discrete pulsing oscillators with different splitting distances and a continuous sweeping oscillator).Results show that there are at least three different velocity peaks in one period at both outlets of continuous-discrete pulsing oscillators. When the splitting distance increases, the first peak velocity (Umax,1,O) decreases, the third one (Umax,3,O) increases, while the second peak velocity (Umax,2,O) is less affected; the three peak velocities generally satisfy Umax,3,O>Umax,1,O>Umax,2,O , unless m˙ is extremely large or small.When the splitting distance increases, oscillating frequency decreases at first and then increases, but the frequency of continuous sweeping oscillator is always the highest and the difference of the other two keeps rising as m˙ increases.Results also show that when the splitting distance was increased or m˙ was reduced to a certain extent, the outlet velocity’s oscillating pattern changes, including the significant velocity fluctuations both before and after Umax,1,O, the phase shift and the great amplitude increase of Umax,2,O.The research results are of great importance in supporting the design optimization of the continuous-discrete pulsing oscillator and the development of flow control method with this kind of fluidic actuators.

CLC number: TP602 Document code: A

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Acta Aerodynamica Sinica
Pages 104-115

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Cite this article:
YANG F, WEN X, HE C, et al. The influence of splitter on the flow dynamics in a continuous-discrete pulsing jet fluidic oscillator. Acta Aerodynamica Sinica, 2023, 41(4): 104-115. https://doi.org/10.7638/kqdlxxb-2022.0147

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Received: 15 September 2022
Revised: 11 November 2022
Published: 04 January 2023
© The journal of Acta Aerodynamica Sinica.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).