journal article·2018-09-01Open access

Analytic Model and the Influence of Actuator Number on the Performance of Plasma Synthetic Jet Actuator Array

Shengfang Huang, Zhibo Zhang, Huimin Song, Yun Wu, Zhengzhong Sun, Yinghong Li

Applied Sciences· Volume 8· Issue 9

Abstract

Coupled with the multichannel discharge model and plasma synthetic jet actuator (PSJA) aerodynamic model, an analytical model to predict the performance of the PSJA array is put forward. The multichannel discharge model takes these factors into consideration, the delay time in the breakdown process, the electrical transformation of the discharge channel from a capacitor to a resistor induced by the air breakdown, and the varying plasma resistance in the discharge process. The PSJA aerodynamic model is developed based on the conservation equations of mass, momentum, energy, and the lumped capacitance method. The multichannel discharge model can simulate the multichannel discharge process and give the discharge energy in the plasma channel. With a constant heating efficiency, the time-independent heating energy deposition power in a discharge channel is obtained. Importing the heating energy, the PSJA aerodynamic model presents the evolution process of the jet. Simulation results show that the jet strength induced by a single actuator decreases with the number of actuators in the PSJA array. When the actuator number increases from 1 to 20, the weakening extent of mass ejected, peak jet velocity, and jet duration time is 62%, 54%, and 33%, respectively. The discharge efficiency increases with the actuator number, while the thermodynamic efficiency decreases with the actuator number. As a result, the total energy efficiency doesn’t always increase with an increase in the number of actuators. When the discharge efficiency of a conventional one channel discharge has been a relatively large value, the total energy efficiency actually decreases with the growth of actuator number.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Plasma and Flow Control in Aerodynamics · Fluid Dynamics and Turbulent Flows · Aerodynamics and Acoustics in Jet Flows

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi'an 710038, China

Institute of Aero-engine, School of Mechanical Engineering, Xi’an Jiaotong University, Xi’an 710049, China

Department of Mechanical Engineering and Aeronautics, City University London, London, UK

Funding

National Natural Science Foundation of China · Royal Society

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