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Investigation of the interaction between NS-DBD plasma-induced vortexes and separated flow over a swept wing
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作者 刘备 梁华 郑博睿 《Plasma Science and Technology》 SCIE EI CAS CSCD 2023年第1期88-99,共12页
The effect of nanosecond pulsed dielectric barrier discharge(NS-DBD) plasma flow separation control is closely related to the actuation frequency,because it involves the interaction between plasma-induced vortexes and... The effect of nanosecond pulsed dielectric barrier discharge(NS-DBD) plasma flow separation control is closely related to the actuation frequency,because it involves the interaction between plasma-induced vortexes and separated flow.In order to study the mechanism of NS-DBD plasma flow separation control over a swept wing,especially the influence of the actuation frequency,at first,experimental studies of the actuation frequencies at 100 Hz are conducted to validate the numerical simulation method.Then,numerical studies of different actuation frequencies which are 50 Hz,100 Hz,160 Hz,200 Hz,500 Hz,and 1000 Hz,respectively are conducted.The interaction between the plasma-induced vortexes and the separated flow is analyzed.Results show that there is a range of the actuation frequency which includes the frequency(160 Hz) calculated by the average aerodynamic chord length to make the control effect good,but when the actuation frequencies are too low(50 Hz) or too high(1000 Hz),the control effect will get worse.The former is because plasmainduced vortexes disappear in a period within an actuation cycle;the latter is because plasma-induced vortexes cannot develop completely,resulting in a weak vortex intensity. 展开更多
关键词 plasma-induced vortex flow separation control ns-dbd LES
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NS-DBD激励控制非细长三角翼前缘涡仿真研究 被引量:6
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作者 赵光银 梁华 +1 位作者 牛中国 王学德 《航空动力学报》 EI CAS CSCD 北大核心 2019年第2期423-433,共11页
通过在三角翼前缘施加纳秒脉冲介质阻挡放电(NS-DBD)激励唯象学模型,进行了47°后掠角钝前缘三角翼流动控制的仿真。分析了不同迎角下升力和阻力系数的变化、流场结构的变化、以及激励诱导旋涡的演化过程。研究表明:施加无量纲激励... 通过在三角翼前缘施加纳秒脉冲介质阻挡放电(NS-DBD)激励唯象学模型,进行了47°后掠角钝前缘三角翼流动控制的仿真。分析了不同迎角下升力和阻力系数的变化、流场结构的变化、以及激励诱导旋涡的演化过程。研究表明:施加无量纲激励频率F+=1.44的NS-DBD激励后,可明显提高三角翼失速前后的升力系数;同时阻力系数也有所增加,变化趋势与实验结果一致。激励在前缘分离剪切层处诱导产生流向涡,改变了前缘剪切层结构,使其向内卷吸;激励后时均流场形成了明显的负压峰值,前缘涡附着线外移,吸力面回流区减小。 展开更多
关键词 等离子体 前缘涡 三角翼 流动控制 纳秒脉冲介质阻挡放电
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Experimental Investigation on Aerodynamic Control of a Wing with Distributed Plasma Actuators 被引量:3
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作者 韩孟虎 李军 +2 位作者 梁华 牛中国 赵光银 《Plasma Science and Technology》 SCIE EI CAS CSCD 2015年第6期502-509,共8页
Experimental investigation of active flow control on the aerodynamic performance of a flying wing is conducted. Subsonic wind tunnel tests are performed using a model of a 35° swept flying wing with an nanosecond... Experimental investigation of active flow control on the aerodynamic performance of a flying wing is conducted. Subsonic wind tunnel tests are performed using a model of a 35° swept flying wing with an nanosecond dielectric barrier discharge (NS-DBD) plasma actuator, which is installed symmetrically on the wing leading edge. The lift and drag coefficient, lift-to- drag ratio and pitching moment coefficient are tested by a six-component force balance for a range of angles of attack. The results indicate that a 44.5% increase in the lift coefficient, a 34.2% decrease in the drag coefficient and a 22.4% increase in the maximum lift-to-drag ratio can be achieved as compared with the baseline case. The effects of several actuation parameters are also investigated, and the results show that control efficiency demonstrates a strong dependence on actuation location and frequency. Furthermore, we highlight the use of distributed plasma actuators at the leading edge to enhance the aerodynamic performance, giving insight into the different mechanism of separation control and vortex control, which shows tremendous potential in practical flow control for a broad range of angles of attack. 展开更多
关键词 PLASMA flow separation control ns-dbd flying wing sequence
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纳秒脉冲等离子体激励控制短舱侧风流动分离实验研究
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作者 张东盛 梁华 +4 位作者 方雨霖 杨鹤森 苏志 张传标 刘诗敏 《空军工程大学学报》 CSCD 北大核心 2023年第2期42-50,共9页
短舱进气道在侧风工作状态下会发生流动分离,导致发动机进气畸变,甚至造成发动机喘振。等离子体流动控制技术在改善流场特性领域具有自身独特的发展优势,其主要难点在于等离子体激励能否与流场产生有效耦合作用实现流动控制目标,而高压... 短舱进气道在侧风工作状态下会发生流动分离,导致发动机进气畸变,甚至造成发动机喘振。等离子体流动控制技术在改善流场特性领域具有自身独特的发展优势,其主要难点在于等离子体激励能否与流场产生有效耦合作用实现流动控制目标,而高压脉冲等离子体技术以其功耗相对较低、对流场持续产生扰动等优势,在控制翼型/机翼流动分离中已取得显著成果,在短舱流动分离控制中存在巨大的潜力。首先探究了侧风影响下短舱进气道的基准气动规律,定量分析总压畸变程度,从而确定了等离子体激励工况,然后采用120°周向激励布局,在不同激励频率电压条件下,进行纳秒介质阻挡放电(NS-DBD)的流动控制效果验证和激励参数影响规律研究。结果表明:施加NS-DBD激励,总压损失系数降低,流动分离范围减小,总压畸变基本消失;随着激励频率的提升,总压畸变程度呈现先减小后增加的趋势;在激励过程中存在一个固有最佳耦合频率,在最佳耦合频率下,总压畸变改善效果最佳;在来流速度为25 m/s,来流偏角为10°的条件下,施加NS-DBD激励,使得平均总压损失系数减小了26.09%,畸变指数减小了31.48%;激励电压阈值上限为10 kV,阈值下限为8 kV;而通过改变激励电压,以改变激励能量的注入,对分离流场改善效果的提升不明显,因此,在实现分离流场控制的同时应尽可能降低激励电压至电压阈值下限,有助于降低能耗、提升寿命,促进等离子体流动控制技术的推广应用。 展开更多
关键词 短舱进气道 流动分离 流动控制 ns-dbd
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Experimental study on plasma actuation characteristics of nanosecond pulsed dielectric barrier discharge 被引量:1
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作者 Hao ZHENG Hua LIANG +4 位作者 Jie CHEN Haohua ZONG Xiangzhe MENG Like XIE Yinghong LI 《Plasma Science and Technology》 SCIE EI CAS CSCD 2022年第1期129-138,共10页
Combining high-speed schlieren technology and infrared imaging technology,related research has been carried out on the influence of parameters such as actuation voltage,repetition frequency,and electrode size of an ac... Combining high-speed schlieren technology and infrared imaging technology,related research has been carried out on the influence of parameters such as actuation voltage,repetition frequency,and electrode size of an actuator on the discharge characteristics,induced flow field characteristics,and thermal characteristics of nanosecond pulsed dielectric barrier discharge.The results show that increasing the value of the actuation voltage can significantly increase the actuation intensity,and the plasma discharge area is significantly extended.Increasing the repetition frequency can increase the number of discharges per unit time.Both will cause more energy input and induce more changes in the flow field.The effect of temperature rise is more significant.The width of the covered electrode will affect the potential distribution during the discharge process,which in turn will affect the extension process of the plasma discharge filament.Under the same actuation intensity,the wider the covered electrode,the larger range the induced flow field and temperature rise is.Preliminary experimental analyses of high-frequency actuation characteristics,temperature field characteristics,flow field characteristics and actuation parameter settings provide support for the parameter selection and partial mechanism analysis of plasma anti-icing. 展开更多
关键词 ns-dbd actuation voltage repetition frequency induced flow field temperature rise
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AC和NS等离子体激励对细长前体分离涡流场的控制 被引量:5
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作者 龙玥霄 李华星 孟宣市 《航空工程进展》 2014年第3期358-363,共6页
为了在更高的风速下实现圆锥前体分离涡的控制,了解AC-DBD和NS-DBD激励器的激励特性,应用交流(AC)放电和纳秒脉冲(NS)放电等离子体激励对20°顶角的圆锥-圆柱组合体圆锥段前体非对称流场进行主动流动控制实验。实验在低速开口风洞... 为了在更高的风速下实现圆锥前体分离涡的控制,了解AC-DBD和NS-DBD激励器的激励特性,应用交流(AC)放电和纳秒脉冲(NS)放电等离子体激励对20°顶角的圆锥-圆柱组合体圆锥段前体非对称流场进行主动流动控制实验。实验在低速开口风洞中进行,迎角45°,风速5~22m/s,流动控制方式为等离子激励器关闭、左舷或右舷等离子体激励器开启三种模式。结果表明:风速5m/s时,通过AC-DBD的左、右舷激励可控制圆锥前体的非对称流场实现镜像对称,NS-DBD则无明显作用效果;随着风速的提高,AC-DBD对非对称载荷的控制作用逐渐减小,与此同时NS-DBD的控制作用逐渐增加;风速22m/s时,NS-DBD可实现圆锥前体非对称流场的镜像对称控制,而AC-DBD则无明显作用效果;相对于AC-DBD等离子体激励,NS-DBD对于更高速度下的分离涡流场控制是有效的。 展开更多
关键词 等离子体控制 细长前体 纳秒脉冲激励器 交流高压激励器 大迎角 主动流动控制
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Comparison of Nitric Oxide Concentrations in μs-and ns-Atmospheric Pressure Plasmas by UV Absorption Spectroscopy
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作者 F.PETERS J.HIRSCHBERG +2 位作者 N.MERTENS S.WIENEKE W.VIOL 《Plasma Science and Technology》 SCIE EI CAS CSCD 2016年第4期406-411,共6页
In this paper,an absorption spectroscopy measurement method was applied on two atmospheric pressure plasma sources to determine their production of nitric oxide.The concentrations are essential for evaluating the plas... In this paper,an absorption spectroscopy measurement method was applied on two atmospheric pressure plasma sources to determine their production of nitric oxide.The concentrations are essential for evaluating the plasma sources based on the principle of the Dielectric Barrier Discharge(DBD)for applications in plasma medicine.The described method is based on a setup with an electrodeless discharge lamp filled with a mixture of oxygen and nitrogen.One of the emitted wavelengths is an important resonance wavelength of nitric oxide(λ = 226.2 nm).By comparing the absorption behaviour at the minimum and maximum of the spectral absorption cross section of nitric oxide around that wavelength,and measuring the change in intensity by the absorbing plasma,the concentration of nitric oxide inside the plasma can be calculated.The produced nitric oxide concentrations depend on the pulse duration and are in the range of 180 ppm to 1400 ppm,so that a distance of about 10 cm to the respiratory tract is enough to conform to the VDI Guideline 2310. 展开更多
关键词 nitric oxide(NO)concentration dielectric barrier discharge(DBD) ultraviolet(UV)absorption spectroscopy plasma medicine pulse duration ns-source μs-source
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