Switching Behavior of a Plasma-Fluidic Actuator
Switching Behavior of a Plasma-Fluidic Actuator
复制标题
等离子体流体致动器的开关行为
DOI:
10.2514/6.2007-785
复制
发表时间:
2007
期刊:
影响因子:
--
通讯作者:
T. McLaughlin
中科院分区:
文献类型:
--
作者:
J. Gregory;Joseph C. Ruotolo;A. Byerley;T. McLaughlin
This work presents the plasma-fluidic actuator as a new type of flow control actuator. The device combines the best features of plasma actuators and fluidic oscillators to create an actuator that decouples the actuation frequency from the flow rate and overcomes the velocity limitations of the plasma actuator. Plasma actuators are used to effectively switch a high momentum jet between Coanda attachment walls by inducing a flow asymmetry across the nozzle of a fluidic oscillator. In this manner the device effectively serves as a fluid amplifier. Switching time, defined as the delay between the plasma initiation and completion of the switching process between opposing attachment walls, is used as a metric to quantify the performance of these new devices. In these tests the jet issuing from the plasma-fluidic actuator was switched between attachment walls in as little as 19 ms. Results indicate that the switching time decreases as the power of the plasma actuator increases. Furthermore, switching times decrease with decreased velocity, as the plasma has more substantial control authority over the primary jet. This new flow control actuator concept has the potential of being used in many applications such as thrust vectoring and jet flow mixing.