|
|
|
题名
|
作者
|
年代
|
出处
|
被引量
|
| 1 | 等离子体合成射流激励器及其流动控制技术研究进展显示文摘等离子体合成射流(PSJ)激励器是通过半封闭容腔内电弧放电的温升及压升作用产生高温高速零质量射流的装置,具有射流速度高、边界层穿透能力强、响应速度快、激励频带宽、无活动部件等优势,是一种应用前景广泛的新型主动流动控制激励器。对等离子体合成射流激励器近些年来的研究进展进行了综述,重点综述了激励器在增大控制能力、提高能量效率、拓展环境适应性等方面所进行的优化设计,介绍了激励器研究中所发展的创新手段,并对激励器的能量效率特性和参数影响规律进行了归纳总结。重点综述了等离子体合成射流激励器在横向主流干扰、分离流控制、激波控制、激波/边界层干扰控制等应用领域的研究进展,深入探讨了等离子体合成射流与横向主流、分离泡、激波等典型流场结构的耦合作用机理,分析了等离子体合成射流主动流动控制存在的动量注入效应、冲击波效应、局部加热效应等复杂作用机制,并对未来的研究方向进行了探讨。 | 周岩 罗振兵 王林 夏智勋 高天翔 谢玮 邓雄 彭文强 程盼 | 2022 | 航空学报2022，43，3： | 22 |
| 2 | 高能电弧等离子体激励控制双压缩拐角激波/边界层干扰实验研究显示文摘超声速/高超声速飞行器进气道入口处多采用多级压缩构型,其诱导的激波/边界层干扰严重影响进气道效率和飞行器的气动性能,因此对双压缩拐角激波/边界层干扰进行流动控制具有较强的应用背景。在来流速度为Ma=2.0的风洞内,针对三种典型的双压缩拐角构型,开展了高能流向脉冲电弧放电阵列调控双压缩拐角激波/边界层干扰的实验研究,并对激励流场的高速纹影图像进行了空间梯度阈值处理和均方根处理。结果显示,在激励的作用下两道分离激波的强度均减弱,验证了利用高能流向脉冲电弧放电阵列控制双压缩拐角激波/边界层干扰的可行性。在分析控制效果的基础上,获得了在不同构型拐角的流场中前驱冲击波列和控制气泡的演化规律,结合控制效果的时序特征,最终揭示了高能流向脉冲电弧放电阵列作用于双压缩拐角激波/边界层干扰的前驱控制和接续控制的接力控制机理。 | 张传标 梁华 郭善广 杨鹤森 刘诗敏 张东盛 | 2022 | 推进技术2022，43，10： | 3 |
| 3 | Modulation of driving signals in flow control over an airfoil with synthetic jet显示文摘A new skill of modulating driving signals of a synthetic jet with low frequency is introduced to enhance the control authority.Based on dynamic mesh technique,the effect of flow control over a NACA0015 airfoil with a Synthetic Jet Actuator(SJA)has been investigated.The SJA is located at x/c=10%,and two jet injection angles of 90°and 30°have been considered.Flow structures indicate that modulation with low frequency can reduce the dissipation rate of vortices after they shed off the surface.Thus aerodynamic performance of the airfoil could be improved.For the injection angle of 90°,modulation can increase the control authority of the SJA.Compared to the unmodulated case,increment of lift-to-drag ratio is up to 15%.The modulating frequency corresponding to the largest increment is F_(M)^(+)≈1.For the injection angle of 30°,improvement of aerodynamic forces positively relates to momentum coefficient of the SJA.Due to the decrease of effective momentum,modulation degrades the effect of flow control.The opposite responses to modulation are believed to have a relationship with the variation of primary control mechanism.When jet injection angle varies from 90°to 30°,the primary mechanism changes from the interaction of vortices and waves to the direct momentum addition.The skill of modulation of driving signals is very useful for applications of SJA. | Zhiyong LIU Zhenbing LUO Qiang LIU Yan ZHOU | 2020 | Chinese Journal of Aeronautics2020，33，12： | 3 |
| 4 | Experimental study on plasma jet deflection and energy extraction with MHD control显示文摘This paper presents an integrated research scheme for vector deflection and energy extraction in a gas plasma jet under Magneto-Hydrodynamic(MHD)control.A MHDcontrolled thrust-vector test rig was used to conduct the experimental research.A gas plasma was obtained by injecting ionization seeds of Cs2CO3 into the combustion chamber via artificially forced ionization.The effects of the gas temperature and ionization seed mass fraction on the plasma jet deflection and energy extraction were experimentally verified under an applied magnetic field.The experimental results were analyzed theoretically.The results showed that the deflection amplitude of the gas plasma jet and the extracted voltage signal intensity increased with increasing gas temperature and the ionization seed mass fraction.The extracted dynamic voltage signals proved that the ionization seeds of Cs2CO3 induced gas ionization at 1173 K.The experiment verified that it is feasible to simultaneously achieve jet deflection and extract energy under the action of an external magnetic field. | Kai ZHAO Ming MING Feng LI Yongji LU Tao ZHOU Kefu WANG Nan MENG | 2020 | Chinese Journal of Aeronautics2020，33，6： | 2 |
| 5 | Experimental investigation on ice-breaking performance of a novel plasma striker显示文摘Aircraft icing has long been a plague to aviation for its serious threat to flight safety.Recently,researches about a newly proposed deicing method based on Plasma Synthetic Jet Actuator(PSJA)have just started.To meet the requirements of in-flight deicing,structure of PSJA needs to be adjusted.This paper completed the detailed design and experimental validation of a novel plasma striker,which was a modified version of PSJA.Influences of mass of the moving part and rod shapes on the ice-breaking performances were also studied.Besides,a“conical-nosed rod configuration”was proposed.Its purpose was to ensure a good ice-breaking performance of the plasma striker on long ice,by generating a splitting failure.Results show that,though mass of the moving part was just several grams,ice-breaking performance was better when the mass was lighter.The rectangular rod could generate an elliptical circumferential crack,whose major axis was parallel to the direction of the long side of the rectangular rod.And the“conical-nosed rod”concept was verified to be able to generate a splitting crack which can spread completely to the far end of long ice,and the crack direction was parallel to edge line of the cone.In general,the plasma striker has the advantages of simple structure,low energy consumption,little harm to the flow field and the aircraft skin.Simulations will be carried out in future works to study in detail the working process of the plasma striker. | Tianxiang GAO Zhenbing LUO Yan ZHOU Shengke YANG Wenqiang PENG Xiong DENG Pan CHENG | 2022 | Chinese Journal of Aeronautics2022，35，1： | 2 |
| 6 | Flow field generated by a dielectric barrier discharge plasma actuator in quiescent air at initiation stage显示文摘A single Dielectric Barrier Discharge(DBD) plasma actuator driven by Alternating Current(AC) power, capable of inducing a starting vortex and a wall jet in quiescent air, is suited for low-Reynolds-number flow control. However, the starting vortex and the wall jet are usually observed after the plasma actuator has been operated for dozens of and hundreds of cycles of the voltage, respectively. The detail of the induced flow field at the initiation stage of the plasma actuator has rarely been addressed. At the initiation stage, a thin jet that provides the impetus for the entrainment of the induced flow at the beginning of the plasma actuation is first observed by using a high-accuracy phase-lock Schlieren technique and a high-speed Particle Image Velocimetry(PIV) system. This is the initial form of the momentum transfer from the plasma to the fluid.Then, an arched type jet is created by the plasma actuator. In addition, the whole development process of the induced flow field from the starting point of the thin jet to the quasi-steady stage of wall jet is presented for providing a comprehensive understanding of the plasma actuator and proposing a relevant enhancement of the numerical simulation model. | Xin ZHANG Y.D.CUI Chien Ming Jonathan TAY B.C.KHOO | 2021 | Chinese Journal of Aeronautics2021，34，3： | 0 |
| 7 | 补气式等离子体合成射流激励器工作机制显示文摘补气式等离子体合成射流(PSJ)激励器通过在常规激励器的腔体上外接单向阀,增加吸气复原阶段的补气量,提升射流能量。为防止漏气,对单向阀结构进行了特别设计,并在单向阀进气口打开和封闭时,分别测量了激励器射流峰值速度、腔体内部压力,及其放电电压和电流,探究单向阀补气改善射流性能的工作机制。结果表明,单向阀能够显著提高等离子体合成射流性能。射流穿透高度提升达30.0%,射流峰值速度增加达到18.7%,射流作用范围面积扩大达76.3%。但其有效作用频段仍与单向阀的响应频率和承受反向冲击压力的能力及激励器饱和工作频率密切相关。补气工作机制是单向阀补气与放电之间形成正向反馈作用,通过单向阀在吸气复原阶段扩大进气口面积,吸气复原更充分,腔内气压增大,使得气体击穿电压升高,增大能量沉积阶段的放电能量,提高腔内压力,产生更大内外压差,从而提升射流性能。射流喷出后腔内负压更大,也进一步促进了吸气复原,通过单向阀补气的作用更显著。 | 刘汝兵 韦文韬 李飞 林麒 | 2022 | 航空学报2022，43，8： | 0 |
您所在的机构暂未开通此部分的功能，请联系管理员