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1.
在Ma=0.4的来流条件下, 利用安装在主翼后缘处的合成双射流激励器对襟翼上的流动进行控制, 在风洞中开展了合成双射流对下游声压级影响的研究. 基于脉动压力测量结果, 结合油流显示试验, 得到了合成双射流对下游不同流动状态区域声压级影响的一些结论. 对于附着流, 在其峰值频率附近激励会明显提高其声压级; 对于受旋涡主导的流动, 恰当的合成双射流控制可以降低声压级, 激励频率较为关键. 在俯仰运动过程中, 对于附着流, 激励提高了声压级, 但不改变其迟滞特性; 对于受旋涡主导的流动, 激励对声压级的影响与攻角有关, 能够减弱其迟滞特性, 但激励强度对迟滞特性的影响较小, 减小声压级的最佳激励与运动历程有关.   相似文献   

2.
为研究结冰环境中热合成双射流激励器工作特性,采用离散相模型(discrete phase model,DPM),结合动网格方法,数值研究了结冰环境中来流速度、液滴含量、液滴直径对激励器工作特性的影响.结果表明,来流速度较小时,双射流激励器出口形成热合成射流融合区,由于热射流的加热作用,温度较高,环境中的过冷液滴难以进入...  相似文献   

3.
等离子体合成射流控制技术因其具有不需要外部气源、工作频带宽、射流速度高、射流净质量通量为零、低功耗、激励器形式多样、环境适应性强等特点,成为了目前针对高速流场主动流动控制技术中应用潜能大、有望实现实际工程应用突破的流动控制装置.传统的等离子体激励器的出口多为垂直于流向或与流向成一定夹角,故垂直于流向的动量分量会对激励器的流动控制能力产生影响.为增强流向动量注入能力,拟设计一种新型的水平动量注入型等离子体合成射流激励器.主要内容有:采用外部电路电参数测量与高速纹影技术,对激励器常压下单周期工作特性与重频工作特性进行了初步研究.对水平动量注入型等离子体合成射流激励器的射流结构进行了分析,探究了该激励器工作频率对射流流场的流场特性与控制能力的影响.最后在高速纹影测量的基础上,开展了激励器高频工作时均出口动压的研究.实验表明:水平动量注入型激励器单周期射流初始速度达到220 m/s,单周期激波初始速度达到477 m/s.此外,工作频率对于激励器的影响主要体现在对激励器控制范围的影响,当激励器工作频率增高时,在相同位置时激励器的动压输入能力下降.   相似文献   

4.
两电极等离子体合成射流激励器工作特性研究   总被引:4,自引:0,他引:4       下载免费PDF全文
王林  夏智勋  罗振兵  周岩  张宇 《物理学报》2014,63(19):194702-194702
采用放电测量和高速阴影技术对两电极等离子体合成射流激励器工作特性进行了系统实验研究.实验表明:激励器工作击穿电压和放电峰值电流随激励器所处环境压强的降低和放电频率的增大而减小,激励器腔体内的放电过程为火花电弧放电.典型的等离子体合成射流流场包含有一道前驱激波和一股呈蘑菇状的高速射流.在整个射流发展过程中,前驱激波以当地声速恒速传播,不随激励器条件的改变而变化,波的强度则随着激励器出口直径的减小、腔体体积的增大、环境压强的降低和放电频率的升高而减小.激励器腔体体积和放电频率的增加会降低腔内气体的加热效果,并减小射流速度.激励器出口直径和环境压强对射流速度的影响按规律变化且存在最佳值.本文实各验条件下激励器都产生了明显的前驱激波和高速射流,具有实现高速流场主动流动控制的应用潜能.  相似文献   

5.
通过FLUENT软件数值模拟的方法,分别对结明冰、混合冰、霜冰翼型的气动特性进行了研究,分析了合成双射流对改善结冰翼型流动分离的影响规律.结果表明:3种冰形均破坏了翼型的流线型,对翼型的气动力特性有不同程度的影响,其中霜冰对翼型气动力特性影响最小,明冰对翼型气动力特性影响最大,混合冰介于两者之间.开启合成双射流激励器,在小攻角情况下,结冰翼型的气动特性得到了有效的改善.而在大攻角情况下,合成双射流激励器不能完全消除分离涡,但可以推迟分离涡,分离涡厚度增加,分离涡最厚点推后.   相似文献   

6.
等离子体合成射流能量效率及工作特性研究   总被引:6,自引:0,他引:6       下载免费PDF全文
王林  罗振兵  夏智勋  刘冰 《物理学报》2013,62(12):125207-125207
基于等离子体激励器工作过程中气体放电的焦耳加热作用, 并结合局部热力学平衡等离子体物理假设, 开展了等离子体合成射流三维唯象数值研究, 获得了完整工作周期内等离子体合成射流流场发展演变过程. 研究结果表明, 单次能量沉积建立的自维持周期性射流中存在有实现激励器腔体"充分" 回填的最大脉冲工作频率––饱和频率. 大的能量沉积、小的激励器出口直径和相同腔体体积下大的径高比都可以产生速度更高的射流, 而射流速度的提高会伴随有饱和频率的降低. 一个饱和周期内, 最多约有16%的初始腔内气体喷出, 吸气复原仅能实现初始腔体质量90%左右的回填.一个大气压条件下, 容性电源供能的等离子体合成射流激励器电能向气体热能和射流动能的转化效率分别约为5%和1.6%. 关键词: 等离子体激励器 合成射流 能量效率 饱和频率  相似文献   

7.
采用放电测量和光学诊断技术对三电极等离子体合成射流激励器放电特性及流场特性进行了实验研究,分析了放电电容、激励器腔体体积和射流出口直径对三电极等离子体合成射流流场分布及速度特性的影响.实验结果表明:三电极等离子体合成射流激励器放电过程包含触发、放电增强、放电衰减和电弧熄灭4个阶段,表现出典型的欠阻尼放电特征;等离子体合成射流流场包含射流主流、"前驱激波"和复杂的反射波系.放电电容、腔体体积和射流出口直径均存在一阈值,当电容和出口直径小于阈值、腔体体积大于阈值时,"前驱激波"以当地声速(约345 m/s)恒速传播,否则"前驱激波"则以大于345 m/s的速度传播,且与射流速度呈现相同的变化趋势,即随着放电电容和出口直径的增加而增大,随着腔体体积的增加而减小.   相似文献   

8.
将实验测得的电弧放电能量分布规律拟合为理想热源,采用数值仿真方法对一种高频等离子体射流激励器进行参数化研究,探索了激励器出口角度对激励器静特性的影响,并获得了在超声速来流(Ma0=2.0)情况下射流激励器的高速特性。结果显示:当射流出口流通面积相同时射流出口角度越小,激励器沿流向的动量注入能力越强,并且这一规律在高速射流条件的情况下仍然适用。相比静止条件,在超声速来流条件下,射流的动量注入能力更强,影响域更大。  相似文献   

9.
实验研究了水滴在冷表面结冰结霜,以及合成热射流除霜除冰过程.实验中采用-30.0℃的半导体制冷片作为制冷源,将水滴滴在半导体制冷片的标定位置,在水滴完全结冰结霜且形态不再改变后,合成热射流激励器工作.利用电子显微镜观测并记录合成热射流除霜除冰的整个过程.结果显示:合成热射流能够完全除去结霜冰滴表面的霜,并且能将凝固水滴完全融化为透明的水滴.并且与合成双射流除霜效果相比,合成热射流的除霜速度极大增加,并且完全除霜后,冰滴的高度比合成双射流除霜减少20%.   相似文献   

10.
采用实验加仿真方法研究了等离子体合成射流对超声速混合层的影响.使用基于纳米粒子的平面激光散射技术(nanoparticle-based planar laser scattering,NPLS)、粒子图像测速技术(particle image velocimetry,PIV)以及纹影手段获取了单次脉冲对混合层的影响.采用二维数值仿真对布置在不同位置的高频激励器的混合效果以及激励器的性能进行了研究.通过对比有扰动和无扰动的NPLS、PIV以及纹影实验结果,发现等离子体合成射流对超声速混合层有明显的扰动,射流喷出时会产生较强的斜激波.对数值仿真结果的分析表明,等离子体合成射流可以有效地增强混合层的厚度.对比激励器布置在不同位置工况下的混合层厚度,可以看出在激励器隔板末端对混合层的扰动效果最好,混合层对在隔板末端的激励器扰动响应也是最快的.对等离子体合成射流激励器的性能分析表明,在隔板末端的激励器输出的能量最多.通过分析等离子体合成射流的作用过程,可以看出激励器在隔板上下表面布置的作用形式是通过作用来流进而影响混合层,在隔板尾端布置的等离子体合成射流激励器直接作用在混合层上,实现混合增强.  相似文献   

11.
This study attempted to control the radiated exterior noise from a rectangular enclosure in which an internal plate vibrates by acoustic excitation and noise is thus radiated from that plate. Multi-channel active control was applied to reduce the vibration and external radiation of this enclosed plate. A piezoelectric ceramic was used as a distributed actuator for multiple mode control of the vibration and radiated noise in the acoustically excited plate. To maximize the effective control, an approach was proposed for attachment the piezoelectric actuator in the optimal location. The plate and internal acoustic space in the enclosure are coupled with each other. This will change dominant frequency characteristics of the plate and, thus, those of the externally radiated noise. Active noise control was accomplished using an accelerometer attached to the plate and a microphone placed adjacent to that plate as an error sensor under acoustic excitation of sine wave and white noise. It was found that the control of radiated external radiation noise requires a microphone as an error sensor, a sound pressure sensor due to vibration of the plate, differences in the dominant frequency of externally radiated noise, and complex vibration modes of the plate.  相似文献   

12.
徐志坚  张心光  王岩松  刘宁宁 《应用声学》2017,25(12):57-59, 67
摘要:降低汽车空腔的振动,是抑制汽车车内噪声的有效途径之一。以激振器、作动器和控制器等为主要部件,搭建了简化的汽车车内噪声主动控制系统,该系统通过将汽车空腔模型简化为板件,以减弱板件振动为目标,实现了汽车车内噪声主动控制。采用简谐正弦及余弦信号作为激振器发出的激励,用于模拟板件的初始振动,控制器通过采用模糊控制算法直接控制压电陶瓷作动器的振动,压电陶瓷作动器的振动用于抑制板件的振动,完成了汽车车内噪声主动控制系统仿真。仿真结果表明,研究采用的汽车车内噪声主动控制系统,使汽车空腔振动降低23%,为解决由汽车发动机和动力总成的振动所引发的汽车车内噪声问题提供了一个有效途径。  相似文献   

13.
The purpose of this paper is to investigate the compressible turbulent synthetic jet flow characteristics of a dual diaphragm piezoelectric actuator. Experimentally, a flow visualization system was established to obtain the particle streak images scattered from 10-μm red fluorescent spheres for observing the synthetic jet flowfield produced by a dual diaphragm piezo actuator. The centerline velocity of the synthetic jet was also measured by using a hot-wire anemometry system. In the analysis, the computational approach adopted the transient three-dimensional conservation equations of mass and momentum with the moving boundary specified to represent the piezo diaphragm motion. The standard k-∈ two-equation turbulent model was employed for turbulence closure. For the actuator operating at the frequency of 648 Hz, the particle streakline images in the cross-sectional plane visualized a turbulent jet flow pattern in the far-field area. The hot-wire anemometry data indicated that the measured centerline velocity of synthetic jets reached 3.8 m/s at y/d= 50. The predictions were compared with the visualized particle streak images and centerline velocity of the synthetic jet in order to validate the computer code. The numerical simulation revealed the time-periodic formation and advection of discrete vortex pairs. Caused by the outward movement of the piezo diaphragms, air near the orifice was entrained into the actuator cavity when the vortex pairs were sufficiently distant from the orifice.  相似文献   

14.
We study experimentally how plasma actuators operating on the basis of surface barrier high-frequency discharge affect jet noise characteristics. The results of investigations of air jets (100?C200 m/s) have demonstrated that the studied plasma actuators have control authority over the noise characteristics of these jets. An actuator??s effect on the jet in the applied configuration is related to acoustic discharge excitation and to a large extent is similar to the well-known Vlasov-Ginevsky effect. It has been shown that jet excitation in the case of St ?? 0.5 using the barrier-discharge plasma actuator leads to broadband amplification of jet sound radiation. The jet excitation in the case of St > 2 leads to broadband noise reduction if the action is sufficiently intensive.  相似文献   

15.
为了保证电子设备能有足够长的工作寿命并可以在高热流下安全运行, 必须可靠而经济地解决高温设备的散热冷却问题. 为解决狭小空间板翅式翅片强化换热能力有限的问题, 基于纵向涡强化换热理论, 提出了合成双射流与表面微凸起复合结构翅组合散热方法. 利用Fluent数值模拟软件对合成双射流作用下的复合结构翅片内部气体流动特性及其强化换热特性进行了研究. 仿真结果表明表面微凸起复合结构翅片的肋片附近Y方向涡量是传统光滑肋片的2倍以上, 换热性能增加10%. 合成双射流驱动频率在500 Hz时, 具有均匀的温度分布以及更好的散热效果; 合成双射流峰值速度下散热效率更好.   相似文献   

16.
周利生  许欣然 《声学学报》2021,46(6):1250-1259
提出了高灵敏度压电共聚物圆管水听器设计方法,论述了聚(偏二氟乙烯-三氟乙烯)[P (VDF-TrFE)]材料结构与压电特性的关系,利用解析法和有限元法,分析了多振动模式耦合特性对压电共聚物圆管水听器灵敏度响应的影响规律,仿真分析了圆管水听器的耐静水压特性和噪声特性,与相同结构的压电陶瓷和压电均聚物水听器相比,压电共聚物圆管水听器低频段灵敏度分别可提高20 dB和5 dB以上,研制了尺寸为Φ14 mm × 55 mm的压电共聚物圆管水听器样品,经测试,在10 Hz~1 kHz频段内水听器灵敏度响应达到-181.8 dB±1 dB,等效自噪声压低于零级海况海洋环境噪声,与理论模型结果有良好的一致性。结果表明,该设计显著提升了圆管水听器的低频接收灵敏度,并为其耐静水压性能提升提供了思路。   相似文献   

17.
This study was intended primarily to reveal more information about the noise producing mechanisms of supersonic jets. Two identical, small, cold air, supersonic, overexpanded jets were tested at selected angles, varying from parallel to 90 degrees intersecting, and at various distances apart. Schlieren photographs of the jet structure and far field sound data were obtained. Close spacing of the parallel jets caused acoustic attenuation, which reached a maximum at one diameter centerline spacing, where the sound of two jets nearly equals that of a single jet. In every case the intersecting jets merged into a single supersonic jet.The overall sound power level of intersecting jets is generally higher than that of two independent jets, because of the turbulent mixing of the two jet flows. A maximum level is reached when the jets intersect at a point near the middle of the flow region containing repetitive shocks. For the parallel jets and intersecting jets at large separation, the sound levels are lower in the plane containing the jet centerlines. For intersecting jets at small separation, however, this shielding effect is reversed.  相似文献   

18.
This paper describes the practical implementation of a piezoelectric actuator as secondary source for hybrid passive/active broadband sound absorption in a standing-wave tube. This actuator consists of a thin circular aluminium plate driven by a piezoelectric patch and glued to a flexible rubber support. The resulting device has been mounted in a thin metallic ring that fits perfectly to the tube diameter. Passive absorption is afforded by either a porous layer or a microperforated panel, backed by an air gap. Active absorption is accomplished by releasing the sound pressure at a microphone behind the material, using either a loudspeaker or the actuator as secondary source. Results of broadband sound absorption reveal the feasibility of the piezoactuator. Compared to the loudspeaker, this actuator allows to greatly reduce the whole thickness of the hybrid absorber.  相似文献   

19.
In the current paper, which deals with the noise pollution excited by distribution transformers in the living area, a comprehensive treatment scheme is put forward for the purpose of reducing the sound pressure level emitting into the environment. In accordance with the associated test standard, the sound pressure levels of distribution transformer and surrounding environment are not only tested but analyzed as well. The measurements were carried out with the frequency analysis of the 1/3 octave resolution, with the center frequencies at 125 Hz, 250 Hz, 400 Hz, and 500 Hz. As illustrated, on the basis of the measurement results, the frequency of noise at 500 Hz of distribution transformer causes the major noise pollution in the surrounding environment. This measurement result is in line with the noise frequency characteristics of distribution transformer. There are two transmission routes of noise: i) the noise excited by distribution transformer transmits by means of the wall of distribution room, and ii) part of noise spreads through the ground of distribution room. Accordingly, acoustic shield and vibration isolation device are applied for the reduction of the low frequency noise emitted through the above two paths. Aimed at applying the appropriate acoustic material and vibration mounting, the evaluation of the noise reduction and vibration absorption is carried out in accordance with the sound and vibration insulation theory. Following the noise treatment, the transformer and environment noise are measured again. The corresponding findings shed light on the fact that the sound level satisfied the requirement of limits of the ordinance. The proposed noise treatment scheme can be applied to the existing power distribution facilities for controlling the sound levels that reach a point where it is comparatively more unobjectionable.  相似文献   

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