绕空化器通气空化流场的实验研究

本文采用高速全流场显示技术和动态应变式测力系统相结合研究了绕圆盘空化器通气空化流动发展过程和动力特性,讨论了通气量对空化流场形态和阻力的影响。结果表明：随着雷诺数增加,绕空化器的通气空化流场经历了初生空化、带状空化、团状空化,阻力系数不断减小,未发生自然空化时,减阻效果明显;随着通气量增加,绕空化器通气空化流场出现了半...     

绕空化器自然空化流动的研究

本文采用高速全流场显示技术、片光源流动显示技术和应变式测力系统相结合研究了圆盘空化器模型的流场。结果表明:随着来流速度增加,绕圆盘流动经过无空化到初生空化的过渡过程后,出现了初生空化、带状空化和团状空化等不同空化阶段;绕圆盘流动阻力系数不断减小,出现了空化后阻力变化梯度降低;绕空化器的流场波动幅度不断加大,但空化器所受阻力主频基本稳定。     

绕水翼初生游离型空化流动结构

为了研究初生空化流动形态及其紊流流场结构,采用高速录像技术观察了绕Clark-Y型水翼初生空化的空化形态,应用LDV分别测量了无空化和初生空化条件下的紊流流场分布.结果表明,绕水翼小攻角无分离流动区域的初生空化形态呈游离发夹涡型空泡团结构,但其具有和单泡相同的发展过程;初生空化和无空化紊流流场的速度和紊流强度没有发现有规律性的差异,初生游离型空穴的形成与发展过程,对雷诺平均流场没有显著的影响.     

绕Hydronautics水翼空化旋涡的高速录像观察

为了解hydronautics超空化水翼的绕流流场特性,采用高速摄像机等流动显示设备,在空化水洞中针对此种超空化水翼进行了一系列绕流流场显示实验。实验结果表明,绕这种超空化水翼的空化形成与发展,均与产生于翼型前端 (吸力面)和尾端(压力面)的旋涡或二者的结合体:空化涡街有关;空化数的大小,决定了空化涡街形成与溃灭的不同特征;当空化数较低时,涡街中空化旋涡的扩张形成了闭合的超空化区域。     

绕水翼云状空化流动特性的研究

采用高速全流场显示技术分别观测了绕超空化水翼和Clark-Y型水翼的云状空化.结果表明:绕超空化水翼和Clark-Y型水翼的云状空化具有相同的变化过程,即:生成、成长、膨胀、脱落和消失溃灭五种状态,两种空化云流动都具有明显的脱落周期和脱落轨迹.在翼型尾部存在的反方向射流,致使空化旋涡脱落;尽管模型尺度、来流速度和空化数基本相同,但由于超空化水翼与Clark-Y型水翼断面形状不同,使翼型尾部的反方向射流强度不同,故与来流相互作用强度不同,导致绕两种水翼的空化云脱落周期不同.在本文实验条件下,绕超空化水翼空化云和Clark-Y型水翼空化云的脱落频率分别为13.5 Hz和19 Hz.     

绕水翼超空化现象的实验研究

超空化现象由于可被应用于水下运动物体的减阻而重新引起了人们的关注。为了了解超空化流动区域的流动特性,观察了超空化流动区域的流动结构;采用LDV的方法测量了超空化发生时绕水翼的速度分布大小。结果表明,当空化发展到超空化阶段,在流动区域内形成明显的空化和水流两个流动区域。在超空化流动区域内,充满了空泡和水的混合物。靠近界面的区域内,混合液流的流速和主流区域的流速大小基本相同,而在邻近翼型表面的区域内,具有较大的速度梯度。     

绕Hydronautics水翼空化云流动的实验研究

采用高速全流场显示技术和DPIV对空化水翼近壁处的空化云流动形态和运动机理进行了讨论.结果表明:绕Hydronautics翼型的空化云运动是一个准周期性过程:稳定空泡团初生在翼型前部,向翼型后部发展布满整个翼面,在翼型后缘出现汽泡团旋涡,伴随反向运动,最终向下游脱落.当前条件下空泡团旋涡脱落周期约为74 ms.空化区与主流区的交界面上存在较大的速度梯度,一组对涡出现在翼型尾部处交界面上.此外,采用以空泡为示踪粒子的DPIV能够对空化流动流速分布进行有效测量.     

表面涂层对绕水翼空化流动影响的实验研究

本文采用高速全流场显示技术观测了两种涂层对绕Clark-Y型水翼空化流动的影响。研究中,随着空化数的降低,主要观测了绕水翼的初生空化、片状空化、云状空化三个阶段σ=1.50时,绕水翼A的空化流动已经发展至片状空化,绕水翼B的空化流动处于初生空化阶段。σ=1.19时,绕水翼A与水翼B空化流动均处于片状空化阶段,围绕两种模型的空穴长度接近,空泡破裂时形成了大量马蹄涡,水翼A表面的附着型锥状空穴产生了大尺度的涡团。σ=0.7时,绕水翼A和水翼B皆为云状空化阶段,绕水翼A的无量纲空化面积小于水翼B;反向射流导致大尺度涡团周期性脱落,绕水翼A的空化涡团脱落较为整齐,绕水翼B则产生分散的马蹄涡。     

绕水翼片状空化流动结构的数值与实验研究

采用数值与实验相结合的方法研究了水翼片状空化流动结构.实验采用高速录像技术观察了片状卒泡形态,应用LDV测量了翼型周围的湍动能和速度分布;采用N-S方程和基于空泡动力学方程的空化模型计算了绕水翼片状空化流场.结果表明:在片状空化阶段,翼型吸力面上附着很薄的一层透明空泡,空泡彤态呈现于指状;随着空化数的减少,空泡尾部水汽交界面相互作用增强,并且空泡尾部出现大的旋涡,影响了空泡尾部区域压力和速度分布,片状空泡尾部的水汽混合区出现不稳定现象,同时存在小的空泡团脱落.数值模拟得到的水翼片状空化流动现象和实验观察到的结果基本一致,验证了计算模型和数值方法的可靠性.     

非定常粘性空化流动模型及其数值计算

基于气液两相当地均相介质模型,本文给出了一种模拟非定常粘性空化流动的计算模型。认为空化绕流流场中流动介质是一种当地均匀的气液混相物。控制方程采用了应用两相流模型的N-S方程。基于液相和气相的状态方程推导了混合介质密度的表达式。为了保证数值计算的稳定性,控制方程的数值求解采用了TVD-MacCormack格式。为了评价计算模型的可靠性,分别计算了绕台阶和管道水锤的空化流动,所得结果是合理的,说明该方法可以用于空化流动的数值计算。     

Performance evaluation of a novel pilot-scale pinned disc rotating generator of hydrodynamic cavitation

This study investigates hydrodynamic performance of a novel pinned disc rotating generator of hydrodynamic cavitation in comparison with a serrated disc variant on a pilot-scale. Experimental results show that at a given rotational speed and liquid flow rate, the pinned disc generates more intense cavitation (i.e. lower cavitation number, higher volume fraction of vapor and higher amplitude of pressure fluctuations) than the serrated disc, while also consuming less energy per liquid pass (i.e., higher flow rate and pumping pressure difference of water at similar power consumption). Additionally, mechanical and chemical wastewater treatment performance of the novel cavitator was evaluated on an 800 L influent sample from a wastewater treatment plant. Mechanical effects resulted in a reduction of average particle size from 148 to 38 µm and increase of specific surface area, while the oxidation potential was confirmed by reduction of COD, TOC, and BOD up to 27, 23 and 30% in 60 cavitation passes, respectively. At optimal operating conditions and 30 cavitation passes, pinned disc cavitator had a 310% higher COD removal capacity while consuming 65% less energy per kg of COD removed than the serrated disc cavitator. Furthermore, the specific COD-reduction energy consumption of the pinned disc cavitator on the pilot scale is comparable to the best cases of lab-scale orifice and venturi devices operating at much lower wastewater processing capacity.     

Stability of slender axisymmetric ventilated cavities closing on cylindrical hulls

Analytical formulae were proposed to estimate the stability of slender axisymmetric ventilated cavities, which allow calculating the dependences of the critical cavitation number versus vapor cavitation number both for the disc and the slender cavitators. These formulae were applied to calculate the stability curves for different radii of the conical hulls located inside the cavity and different shapes of the cavitator, Froude numbers and directions of the ambient flow.     

The influence of air content in water on ultrasonic cavitation field

Cavitation is a complex physical phenomenon affected by many factors, one of which is the gas dissolved in the medium. Researchers have given some efforts to the influence of gas content on sonoluminescence or some specific chemical reactions in and around the bubble, but limited work has been reported about the influence on the ultrasonic cavitation field distribution. In this work, the intensity distribution of the ultrasound field in a cleaning tank has been measured with the hydrophone. After analysed and visualised by MATLAB software, it was found that the cavitation intensity distribution in degassed water was much better than that in tap water. And further study proved that degassing process can improve the cavitation effect dramatically both in intensity and scope. Finally, the cavitation fields in mediums with different gas content were measured and the specific influence of air content on cavitation field was discussed.     

双泡模型共振频率的超声空化动力学研究

该研究旨在研究双泡模型的自然共振频率对超声空化的影响,通过理论计算研究了自然共振频率的影响因素,以及单频超声和双频超声与自然共振频率的关系。研究结果表明：气泡初始半径是影响自然共振频率的主要因素;低频驱动下的非线性波动程度会比高频的更加剧烈,当驱动频率等于气泡自然共振频率时,超声空化的效果更好;双频超声取气泡自然共振频率时超声空化效果远远优于单频超声驱动。该研究在超声医学和理解超声空化特性方面有着重要的意义。     

Study on mechanism of chitosan degradation with hydrodynamic cavitation

Hydrodynamic cavitation is an effective method for chitosan degradation, of which the mechanism directly determines the molecular weight distribution of degradation products. In this study, based on the Monte Carlo simulation and experimental results, the mechanism of chitosan degradation with hydrodynamic cavitation and molecular weight distribution of products were analyzed. The results showed that the algorithm established in the simulation could effectively analyze degradation mechanism and the factors that influenced degradation mechanism and molecular weight distribution of products. The degradation with hydrodynamic cavitation was caused by chemical and mechanical effects, of which the former dominated the degradation process. The outlet and inlet angles and throat length of the cavitator had major and minor influences on the degradation pattern, respectively. The chemical effect led to random cuts resulting in wide distribution of the products, while the mechanical effect led to central cuts resulting in narrow distribution of the products. With more central cuts, the slide-shaped molecular weight distribution curve of degradation products was gradually transferred into a bell-shaped curve. These results provide instructions for researches on the molecular weight distribution of chitosan products degraded with hydrodynamic cavitation.     

Experimental study on the characteristics of ventilated cavitation around an underwater navigating body influenced by turbulent drag-reducing additives

In this study, a new control strategy for turbulent drag reduction involving ventilated cavitation is proposed. The configurational and hydrodynamic characteristics of ventilated cavities influenced by turbulent drag-reducing additives were experimentally studied in water tunnel. The test model was fixed in the water tunnel by a strut in the aft-part. Aqueous solutions of CTAC/Na Sal(cetyltrimethyl ammonium chloride/sodium salicylate) with weight concentrations of 100, 200, 400 and 600 ppm(part per million), respectively, were injected into the ventilated air cavity from the edge of the cavitator with accurate control by an injection pump. The cavity configurations were recorded by a high-speed CCD camera. The hydrodynamic characteristics of the test model were measured by a six-component balance. Experimental results show that, within the presently tested cases, the lengths of cavity influenced by drag-reducing solution are smaller than normal condition(ventilated cavity) in water, but the asymmetry of the cavity is improved. The drag resisted by the test model is reduced dramatically(the maximum drag reduction can reach to 80%) and the re-entrant jet is more complex after the CTAC solution is injected into the cavity. Turbulent drag-reducing additives have the potential in enhancement of supercavitating asymmetry and further drag reduction.     

三维小空化数空泡流数值方法

采用均质平衡流空泡模型,引入基于求解液体质量份数输运方程的空泡流模型,提出新的压力密度耦合的压缩性方法和控制气液两相转换的源项,求解汽水混合介质的RANS方程和带低雷诺数修正的k-ε模型,实现了小空化数(σ=0.2~0.01)下水下航行体的空泡流数值模拟.得到清晰的空泡形态特征与内部结构,以及空泡长度和最大直径随空化数的变化规律,给出航行体运动阻力系数与空化数之间的变化关系.将计算结果与解析结果及实验数据进行比较表明,该方法保证了极小空化数下自然空泡流计算的稳定性与收敛性,提高了空泡形态特性的预报精度.     

高速水流中旋涡空化所引起的空蚀和振动

为了研究旋涡空化所引起的空蚀和振动观象以及二者的关系,采用高速摄影的方法,观察了发生在射流放水阀山部的空化形态。采用快速富里叶变换（FFT）分析了空化所引起的振动。采用失重法,进行了空蚀实验。结果表明,旋涡空化能引起严重的空蚀和剧烈的振动。在旋涡空化发展的个同阶段,其所导致的振动和空蚀呈观了个同的特性。当Sσ>0.74时,随空化数的变化,振动和空蚀呈现了相同的变化趋势,但是,在0.50<σ<0.74的范围内,振动和空蚀呈现了相反的变化趋势。这是由于水流中空化旋涡的数目和形态随空化数的变化,以及旋涡空化引起振动和空蚀的机理不同所造成的。     

超声空化对丙酮激光喇曼光谱的影响

本研究设计了一种可吸入超声的喇曼光谱样品池,对丙酮的激光喇光曼谱的检测表明,超声空化降低了喇曼光谱的强度,我们认为,超声空化减少了激光光路上参与散射的丙酮分子数是光谱强度降低的主要原因。