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Analytic model and the influence of actuator number on the performance of Plasma Synthetic Jet Actuator Array

机译:解析模型及执行器数量对等离子合成射流执行器阵列性能的影响

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Coupled with the multichannel discharge model and plasma synthetic jet actuator (PSJA) aerodynamic model, an analytic model to predict the performance of the PSJA array is put forward. The multichannel discharge model is developed based on the basic electronic theory. 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 the jet strength induced by a single actuator decreases with the number of actuator 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 increase all the time with the increase of actuator number. When the discharge efficiency of conventional one channel discharge has been a relative large value, the total energy efficiency even decreases with the growth of actuator number.
机译:结合多通道放电模型和等离子体合成射流致动器(PSJA)气动模型,提出了一种预测PSJA阵列性能的解析模型。基于基本电子理论开发了多通道放电模型。基于质量,动量,能量和集总电容法的守恒方程,开发了PSJA空气动力学模型。多通道放电模型可以模拟多通道放电过程,并给出等离子体通道中的放电能量。以恒定的加热效率,获得放电通道中与时间无关的加热能量沉积功率。通过输入热能,PSJA空气动力学模型展示了射流的演变过程。仿真结果表明,单个致动器引起的喷射强度随PSJA阵列中致动器数量的增加而降低。当执行器数量从1增加到20时,喷射质量的减弱程度,峰值喷射速度和喷射持续时间分别为62%,54%和33%。排放效率随执行器数量的增加而增加。同时,热力学效率随执行器数量的增加而降低。结果,总能量效率不会一直随着执行器数量的增加而增加。当常规的单通道放电的放电效率已经是相对较大的值时,总能量效率甚至随着致动器数目的增加而降低。

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    Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi'an, 710038, People ' s Republic of China United Kingdom;

    Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi'an, 710038, People ' s Republic of China United Kingdom;

    Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi'an, 710038, People ' s Republic of China United Kingdom;

    Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi'an, 710038, People ' s Republic of China United Kingdom;

    Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi'an, 710038, People ' s Republic of China United Kingdom;

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