Recent advances in shock wave boundary layer interaction research are reviewed in four
areas:(i) understanding low frequency unsteadiness,(ii) heat transfer prediction …

In an air-breathing engine the flow deceleration from supersonic to subsonic conditions
takes places inside the isolator through a gradual compression consisting of a series of …

The interaction between a ramp induced shock wave and a plasma synthetic jet actuator
(PSJA) array was experimentally investigated using high-speed schlieren imaging …

Spark discharge plasma synthetic jets (SPJs) have been used for the active flow control
study on an NACA 0021 straight-wing model in a wind tunnel. The model forces and …

In the field of flow control research, oblique jets are known to offer several advantages over
vertical jets. To gain a comprehensive insight into the flow field characteristics of a plasma …

The plasma synthetic jet (PSJ) is a high-energy synthetic jet that is excited by gas spark
discharging plasma in an active flow-control area. Because achieving large-scale flow …

为考察火花放电等离子体射流控制机翼气动力矩的效果, 在NACA0021 平直机翼模型上安装
火花放电等离子体射流发生器, 通过改变射流发生器安装位置, 射流角度及加载电参数 …

针对高超声速进气道激波与边界层干扰流动分离控制问题, 提出了一种低功率重频非定常激励
方式, 并基于雷诺平均Navier-Stokes (NS) 方程, 从唯象学的角度出发, 将等离子激励简化为功率 …

A plasma synthetic jet actuator with a high-frequency oblique slot was designed for
supersonic flow control. The actuator's periodic operation characteristics were investigated …

提出一种火花放电等离子体射流发生器, 可获得能量较高的零质量射流. 其工作频率可达9kHz,
可在大气压下产生持续的平均速度较高的射流. 详细阐述了该射流发生器结构; …