执行机构
等离子体驱动器
流量控制(数据)
流体学
计算机科学
控制工程
气动执行机构
流量(数学)
工程类
航空航天工程
电气工程
人工智能
物理
电压
介质阻挡放电
机械
计算机网络
作者
Louis N. Cattafesta,Mark Sheplak
标识
DOI:10.1146/annurev-fluid-122109-160634
摘要
Actuators are transducers that convert an electrical signal to a desired physical quantity. Active flow control actuators modify a flow by providing an electronically controllable disturbance. The field of active flow control has witnessed explosive growth in the variety of actuators, which is a testament to both the importance and challenges associated with actuator design. This review provides a framework for the discussion of actuator specifications, characteristics, selection, design, and classification for aeronautical applications. Actuator fundamentals are discussed, and various popular actuator types used in low-to-moderate speed flows are then described, including fluidic, moving object/surface, and plasma actuators. We attempt to highlight the strengths and inevitable drawbacks of each and highlight potential future research directions.
科研通智能强力驱动
Strongly Powered by AbleSci AI