论文标题
通过强烈非平衡脉冲等离子体中的超快速局部加热来控制煤气流量
Gasdynamic Flow Control by Superfast Local Heating in a Strongly Nonequilibrium Pulse Plasma
论文作者
论文摘要
纸张使用高度非平衡性脉冲等离子体中的热量释放对现代作品进行了现代作品的评论。主要注意力是基于超快(大气压下的纳秒时间尺度上)的局部加热的效果,因为目前,使用气体排放的高速流量控制中的主要成功与这种热效应有关。详细考虑了控制放电与气流相互作用的物理机制。审查的第一部分简要介绍了脉冲局部能量沉积的血浆空气动力学方法中最流行的方法:纳米秒表面屏障放电,脉冲火花放电以及纳米秒/飞秒激光放电。分析了在这些放电中以及放电血浆衰减期间,在高电场上的超快加热的机制。评论的第二部分包含了众多对气体流动流的血浆控制的例子。冲击波在超音速对象前的控制和控制轨迹的控制;控制分离的流和层的控制;控制层扰动过渡的控制;边界层以大攻击角度控制边界层的静态和动态分离;以及在各种天气条件下血浆致动器的操作;并分析了血浆作为抗冰淇淋工具的使用。
Paper presents a review of modern works on the gasdynamic flow control using a heat release in highly nonequilibrium pulsed plasma. The major attention is paid to the effects based on ultrafast (on nanosecond time scale at atmospheric pressure) local heating of the gas, since at present the main successes in high-speed flow control using gas discharges are associated with namely this thermal effect. The physical mechanisms that control the interaction of the discharges with gas flows are considered in detail. The first part of the review briefly describes the most popular approaches in plasma aerodynamics for the pulsed localized energy deposition: nanosecond surface barrier discharges, pulsed spark discharges, and nanosecond/femtosecond laser discharges. The mechanisms of ultrafast heating of air at high electric fields realized in these discharges, as well as during the decay of a discharge plasma, are analyzed. The second part of the review contains numerous examples of plasma control of gasdynamic flows. The control of the shock waves configuration in front of a supersonic object and control of its trajectory; the control of quasistationary separated flows and layers; the control of a laminar-turbulent transition; the control of static and dynamic separation of the boundary layer at large angles of attack; as well as the operation of plasma actuators in various weather conditions; and the use of plasma as an anti-icing tool for flying objects are analyzed.