Flow control using surface Dielectric Barrier Discharge (DBD) plasma actuators driven by a
sinusoidal alternating-current power supply has gained significant attention from the …

Ice accretion is a common issue on aircraft flying in cold climate conditions. The ice
accumulation on aircraft surfaces disturbs the adjacent airflow field, increases the drag, and …

层流控制, 复合材料, 全电驱动等创新性航空技术的应用给传统防/除冰方法带来了新的挑战.
基于高电压驱动的表面介质阻挡放电等离子体激励新概念防/除冰方法因其没有复杂的机械构造 …

正弦交流介质阻挡放电等离子体流动控制技术是基于等离子体激励的主动流动控制技术,
具有响应时间短, 结构简单, 能耗低, 不需要额外气源装置等优点, 在飞行器增升减阻, 抑振降噪 …

In the present study, we report for the first time the observations of the melting process of an
ice bead under the thermal effects of the AC-DBD plasma actuator. The melting process of …

Icing and stalling on the surfaces of aircraft wings endanger flight safety. The object of this
research is a nanosecond pulsed dielectric-barrier-discharge plasma actuation unit with a …

Navier–Stokes computations are performed, and detailed results are documented on the
vortex shedding, lift and drag fluctuations, and their spectra for flow past a square cylinder …

In order to improve the aerodynamic performance of the wing at post-stall conditions, the
experimental comparative investigations on the flow separation control over an ONERA 212 …

Flow control technology using dielectric barrier discharge plasma actuators which are driven
by a sinusoidal alternating current high-voltage power is an active flow control technology …

Flow control technology using the pulsed-DC plasma actuators has been demonstrated as
an effective way of reducing the turbulent boundary-layer drag, which has attracted great …