• Title/Summary/Keyword: Sparkjet Actuator

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Research on Flow Analysis Program Development Considering Equilibrium Plasma Flow and Impulse Characterization of Sparkjet Actuator (플라즈마에 의한 평형 유동을 고려한 스파크제트 액츄에이터 유동 해석 프로그램 개발과 추력 특성 연구)

  • Kim, Hyung-Jin;Shin, Jin Young;Chae, Jeongheon;Ahn, Sangjun;Kim, Kyu Hong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.2
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    • pp.90-97
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    • 2019
  • Sparkjet actuator, also known as plasma synthetic jet actuator (PSJA), is an active flow control device that has possibility of controling supersonic flow. This actuator utilizes arc plasma to deposit energy onto the gas inside the cavity to raise temperature and pressure. A change in the state of the fluid inside the cavity generates pressure waves and momentum jet, and they are exhausted through out the orifice exit and disturb external flow field. Since the cavity flow is affected by arc plasma, which is an equilibrium plasma and have generated equilibrium flow, the equilibrium state of air should be considered in order to analyze the flow of sparkjet actuator. In this study, numerical program for equilibrium flow was developed for the use of sparkjet actuator analysis. The developed program was validated by comparing the time - accurate jet front positions with the reference result. Then, impulse characteristics of the actuator in the atmospheric quiescent air were explained.

Influence of Electrode Position on Performance of Sparkjet Actuator Using Numerical Analysis (수치해석을 이용한 전극 위치에 따른 스파크제트 액츄에이터의 성능 연구)

  • Shin, Jin Young;Kim, Hyung-Jin;Kim, Kyu Hong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.11
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    • pp.753-760
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    • 2019
  • Sparkjet actuator, also known as plasma synthetic jet actuator, which is a kind of active flow control actuator is considered as being high possibility for the supersonic flow control due to ejecting stronger jet compared to the other active flow control actuators. Sparkjet actuator generates high temperature and high pressure flow inside the cavity by using arc plasma and leads momentum by ejecting such flow through orifice or nozzle. In this research, numerical calculation of sparkjet actuator with respect to the location of electrodes which exists inside the cavity is conducted and the change of the performance of sparkjet actuator is suggested. As the location of electrodes goes closer to the bottom of the cavity, impulse is increased and the average pressure inside the cavity maintains higher. When the location of electrode is 25% and 75% of the entire cavity height, impulse is 2.515 μN·s and 2.057 μN·s, respectively. Each impulse is changed by about 9.92% and -10.09% compared to when the location of electrodes is 50% of the entire cavity height.