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Effect of noncircular orifice plates on the near flow field of turbulent free jets
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作者 徐敏义 童杏清 +4 位作者 岳丹婷 张健鹏 米建春 Nathan G.J. Kalt P.A.M. 《Chinese Physics B》 SCIE EI CAS CSCD 2014年第12期298-306,共9页
In this paper, we experimentally investigate the near-field flow characteristics of turbulent free jets respectively issued from circular, triangular, diamond, rectangular, and notched-rectangular orifice plates into ... In this paper, we experimentally investigate the near-field flow characteristics of turbulent free jets respectively issued from circular, triangular, diamond, rectangular, and notched-rectangular orifice plates into air surroundings. All the orifice plates have identical opening areas or equivalent diameters(De) and their aspect ratios(AR) range from 1 to 6.5. Planar particle image velocimetry(PIV) is used to measure the velocity field at the same Reynolds number of Re = 5 × 10^4,where Re = Ue De/ν with Ue being the exit bulk velocity and ν the kinematic viscosity of fluid. The mean and turbulent velocity fields of all the five jets are compared in detail. Results show that the noncircular jets can enhance the entrainment rate, reflected by the higher acceleration rates of mean velocity decay and spread, shorten the length of the unmixed core,expedite the increase of turbulent intensity compared with the circular counterpart shortened unmixed core, and increase turbulent intensity comparing to the circular counterpart. Among the five jets, the rectangular jet(AR = 6.5) produces the greatest decay rate of the near-field mean velocity, postpones the position at which the 鈥榓xis-switching鈥檖henomenon occurs. This supports that axis switching phenomenon strongly depends on jet initial conditions. In addition, the hump in the centerline variation of the turbulence intensity is observed in the rectangular and triangular jets, but not in the circular jet, nor in diamond jet nor in notched-rectangular jet. 展开更多
关键词 noncircular jet free jet turbulence mixing axis-switching
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PSEUDOSPECTRAL ANALYSIS OF THE INTERFACIAL STABILITY OF FREE JETS WITH DIFFERENT VELOCITY PROFILES
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作者 苏海容 胡国辉 周哲玮 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2004年第12期1323-1332,共10页
A double fluid model for a liquid jet surrounded by a coaxial gas stream was constructed. The interfacial stability of the model was studied by Chebyshev pseudospectral method for different basic velocity profiles. Th... A double fluid model for a liquid jet surrounded by a coaxial gas stream was constructed. The interfacial stability of the model was studied by Chebyshev pseudospectral method for different basic velocity profiles. The physical variables were mapped into computational space using a nonlinear coordinates transformation. The general eigenvalues of the dispersion relation obtained are solved by QZ method, and the basic characteristics and their dependence on the flow parameters are analyzed. 展开更多
关键词 free jet Chebyshev pseudospectral method interfacial stability
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Experimental Investigation of the Cooling Capacity of Gaseous Carbon Dioxide in Free Jet Expansion for Use in Portable Air-Cooling Systems
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作者 Chady Al Sayed Ludwig Vinches Stéphane Hallé 《Open Journal of Applied Sciences》 2018年第2期62-72,共11页
This paper investigates the possibility of using the free expansion of gaseous CO2 in portable air-cooling systems. The cooling capacity of the gaseous CO2 free jet expansion was calculated using three different appro... This paper investigates the possibility of using the free expansion of gaseous CO2 in portable air-cooling systems. The cooling capacity of the gaseous CO2 free jet expansion was calculated using three different approaches and the results showed that the simplified calculations would give approximated cooling values with an 11.6% maximum error. The mass flow rate, upstream pressure and cooling capacity of the gaseous CO2 decreased with time. A maximum 48.5 watts of cooling was recorded at minute 4 and a minimum value of 10.4 watts at the end of the test. The drop in cooling capacity is due to the evaporation of the liquid CO2 inside the small cylinder which cools the two-phase CO2 mixture and causes a pressure drop (from 6 MPa to 2.97 MPa), which also affects the mass flow rate of gaseous CO2 exiting the orifice (from 0.56 g/s to 0.24 g/s). If this cooling technique is to be considered in portable compact-cooling systems, the mass, pressure and cooling capacity drop with time must be solved. One of the solutions could be to cover the cylinder with a heating coat to compensate for the heat absorbed by the evaporation of the liquid CO2. 展开更多
关键词 Gaseous CO2 free jet EXPANSION COOLING Capacity Compact Air-Cooling Technique
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Experiment and Numerical Simulation of Free Water Jet by a Central-body Nozzle 被引量:3
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作者 YANG Minguan ZHANG Feng +1 位作者 KANG Can GAO Bo 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2010年第6期797-804,共8页
The recent research about cavitation jet mainly focuses on the organ-pipe nozzle and triangular nozzle.The research content mainly includes the optimized design about the structure of nozzles,the observation and flow ... The recent research about cavitation jet mainly focuses on the organ-pipe nozzle and triangular nozzle.The research content mainly includes the optimized design about the structure of nozzles,the observation and flow analysis about the cavitation jet in the water,and the theory of rock attacked by the cavitation jet,while the energy characteristic of the free jet is not studied yet.In China,the research about the central-body nozzle is almost empty.For the purpose of studying the energy characteristic and the structure of free water jet discharged from central-body nozzle,an experiment with phase Doppler particle anemometry(PDPA)technology is carried out to measure the free water jet flow,which is produced by a central-body nozzle under the jet pressure of 15 MPa.While five sections with different axial distances from the nozzle outlet are selected for data process and analysis,the axial and radial velocity and the droplets of the particle size are studied.Meanwhile,numerical calculation of corresponding flow field is conducted by using volume of fluid(VOF)multiphase model,and the jet flow feature is discussed.The experimental and calculating results show that the axial velocity of high speed jet flow dissipates slowly in the air,and the core area and diffused area are discovered.The diameter of droplet in the core area is small,and jet energy is concentrated,while in the diffusion area,water is mingled with ambient air and radial velocity is relatively large.Obvious low-pressure area exists behind the central body and potential cavitation may occur in that area.The proposed research reveals the energy characteristic of free jet discharged from central-body nozzle,provides the theoretical basis for preestimating erosion feature of the central-body nozzle and also the theoretical foundation for revealing the mechanism of erosion. 展开更多
关键词 central-body nozzle free water jet phase Doppler particle anemometry(PDPA) energy characteristic VOF model
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Analysis on MHD Stability of Free Surface Jet flow in a Gradient Magnetic Fields
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作者 许增裕 康伟山 潘传杰 《Plasma Science and Technology》 SCIE EI CAS CSCD 2004年第3期2301-2306,共6页
The simplified modeling for analysis on MHD stability of free surface jet flow in a gradient magnetic fields is based on the theoretical and experimental results on channel liquid metal MHD flow, especially, the resul... The simplified modeling for analysis on MHD stability of free surface jet flow in a gradient magnetic fields is based on the theoretical and experimental results on channel liquid metal MHD flow, especially, the results of MHD flow velocity distribution in cross-section of channels (rectangular duct and circular pipe), and the expected results from the modeling are well agreed with the recent experimental data obtained. It is the first modeling which can efficiently explain the experimental results of liquid-metal free surface jet flow. 展开更多
关键词 free surface jet flow MHD stability MODELING
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Mixing and initiating mechanism of internal injection oblique detonation engine
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作者 Jingyu ZHANG Guoqiang HE +3 位作者 Yunfeng LIU Fei QIN Xianggeng WEI Shaohua ZHU 《Chinese Journal of Aeronautics》 2026年第2期115-122,共8页
This paper presents the results of free-jet experiments conducted on an internal injection oblique detonation engine in a large-scale hypersonic shock tunnel.To overcome the challenges of non-uniform mixing and the fa... This paper presents the results of free-jet experiments conducted on an internal injection oblique detonation engine in a large-scale hypersonic shock tunnel.To overcome the challenges of non-uniform mixing and the failure of oblique detonation wave initiation when using liquid fuel,a combined strut-wall injection configuration was employed.Initiation was achieved by introducing a bump structure on the wedge.The results demonstrate that this strategy for mixing and initiation effectively establishes the oblique detonation wave combustion flow field.To further investigate the fuel mixing and initiation processes in the oblique detonation engine,three-dimensional numerical simulations consistent with the experimental conditions were carried out using the ReynoldsAveraged Navier-Stokes(RANS)method.The simulation results reveal that the high-speed gas flow generates shock waves as it passes through the central strut and transverse fuel jets.These shock waves are reflected by the wall,forming a series of shocks in the mixing section.The kerosene injected from the strut injectors does not react during the mixing phase.However,due to the influence of the high-temperature boundary layer,the kerosene injected through the wall undergoes precombustion.The separation zone upstream of the bump generates separation shock waves,allowing the multi-wave point to stabilize at a short distance from the leading edge of the wedge. 展开更多
关键词 Blunt bump free jet test Liquid kerosene Oblique detonation engine Pre-combustion Strut-wall combined injection
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自由圆湍流射流流动及卷吸特性研究
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作者 段鼎立 葛海涛 +3 位作者 辛宇航 奚修智 杨竹强 张博 《热科学与技术》 北大核心 2026年第1期69-77,共9页
基于FLUENT对亚音速自由圆湍流射流进行数值模拟研究,改变直喷嘴进口压力和收缩喷嘴收缩角度,研究射流的流动和卷吸特性。研究结果表明:射流锥角对压力和收缩喷嘴收缩角度不敏感,相同轴向位置上的速度厚度和涡量厚度相差不大,最大偏差为... 基于FLUENT对亚音速自由圆湍流射流进行数值模拟研究,改变直喷嘴进口压力和收缩喷嘴收缩角度,研究射流的流动和卷吸特性。研究结果表明:射流锥角对压力和收缩喷嘴收缩角度不敏感,相同轴向位置上的速度厚度和涡量厚度相差不大,最大偏差为1.1 mm,速度厚度及涡量厚度增长率均维持在12%~16%;直喷嘴射流卷吸率随压力的升高不断降低,两者的变化满足二次函数关系;改变喷嘴形式,将直喷嘴改为收缩喷嘴,卷吸率大幅度增加,增幅可达16.0%,但是收缩喷嘴收缩角度则对卷吸率影响不大。 展开更多
关键词 自由射流 射流锥角 边界层厚度 卷吸率
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自由射流中类孤立波相干结构的Reynolds数效应
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作者 胡子渊 蔡庆东 杨延涛 《气体物理》 2026年第1期13-24,共12页
为探究Reynolds数对圆管自由射流中类孤立波相干结构(soliton-like coherent structures,SCS)的调控机理,在Reynolds数2000~6600范围内开展了一系列直接数值模拟。结果显示,Reynolds数变化虽未改变时均射流的整体结构,但显著影响其动量... 为探究Reynolds数对圆管自由射流中类孤立波相干结构(soliton-like coherent structures,SCS)的调控机理,在Reynolds数2000~6600范围内开展了一系列直接数值模拟。结果显示,Reynolds数变化虽未改变时均射流的整体结构,但显著影响其动量输运:低Reynolds数下射流中心线速度衰减更快,但径向扩展更缓。在所有工况下,SCS均出现于高、低速交错区,其核心的类孤立波结构形态在不同Reynolds数下保持稳定,且越靠近射流中心,SCS形成位置越早、振幅越大、数量越多。随着Reynolds数升高,SCS的出现位置总体向上游移动,数量增多。Lagrange物质面追踪和相关性分析证实,SCS具备类孤立波性质,且发展过程中会诱导两侧剪切层中旋涡生成,而高Reynolds数下,SCS更早失稳并破碎。研究表明,Reynolds数虽未改变SCS的核心类孤立波结构形态,但通过调控流动的惯性效应与黏性耗散平衡,系统地影响了其生成位置、数量、稳定性等演化参数,进而塑造了自由射流的转捩路径。 展开更多
关键词 自由射流 类孤立波相干结构 直接数值模拟 Lagrange示踪 相关性分析
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3D MHD Jet in a Non-Uniform Magnetic Field 被引量:1
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作者 黄护林 韩东 《Plasma Science and Technology》 SCIE EI CAS CSCD 2005年第6期3092-3096,共5页
The purpose of this paper is to present a two-phase 3D magnetohydrodynamics (MHD) flow model that combines the volume of fluid (VOF) method with the technique derived from induced-magnetic-field equations for liqu... The purpose of this paper is to present a two-phase 3D magnetohydrodynamics (MHD) flow model that combines the volume of fluid (VOF) method with the technique derived from induced-magnetic-field equations for liquid metal free surface MHD-jet-flow. Analogy between the induced-magnetic-filed equation and the conventional computational fluid dynamics (CFD) equation is made, so that the equation can be conveniently accounted for by CFD. A penalty factor numerical method is introduced in order to force the local divergence-free condition of the magnetic fields and an extension of the void insulating calculation domain is applied to ensure that the induced-magnetic field at its boundaries is null. These simulation results for lithium liquid metal jets under magnetic field configurations of Magnetic Torus (Mtor) and National Spherical Torus Experiment (NSTX) outboard divertor have shown that three dimensional jet can not be annihilated by magnetic braking and its cross-section will deform in such a way that the momentum flux of the jet is conserved. 3D MHD effects from a magnetic field gradient cause return currents to interact with applied magnetic fields and produce unfavorable Lorentz forces. Under 3D applied non-uniform magnetic fields of the divertor, unfavorable Lorentz forces lead to a substantial change in flow pattern and a reduction in flow velocity, with the jet cross-section moving to one side of the jet space. These critical phenomena can not be revealed by 2D models. 展开更多
关键词 magnetohydrodynamics MHD induced-magnetic-equation free jet volume of fluid (VOF) method free surface
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The Numerical Simulation of Flow Field of Jet System
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作者 Guo Jinji, Zhang Sheng and Chen TongMechanics Dept. of Zhongshan University,Guangzhou 510275. China 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 1993年第3期62-69,共8页
In this paper, the internal fluid motion of a jet system is described by the Navier Stokes mechanics equations. For the simulation of the motion, the penalty function finite element method is used, and the velocity ve... In this paper, the internal fluid motion of a jet system is described by the Navier Stokes mechanics equations. For the simulation of the motion, the penalty function finite element method is used, and the velocity vectors and stream function curves are obtained. Using the Prandtl theory, this paper derives the free jet velocity and the jet bunch width in a half-space, the latter of which is amended by experiment. The results obtained in this paper are applied to micro-type high pressure water jet cleaner and the ejector of rocket engine. 展开更多
关键词 Fluid mechanics equations Penalty finite element method Numerical simulation free jet jet bunch width.
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采用DC Arc Plasma JetCVD方法沉积微/纳米复合自支撑金刚石膜 被引量:3
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作者 戴风伟 陈广超 +7 位作者 兰昊 J.Askari 宋建华 李成明 佟玉梅 李彬 黑立富 吕反修 《人工晶体学报》 EI CAS CSCD 北大核心 2006年第6期1200-1202,1208,共4页
在30kW级直流电弧等离子体喷射化学气相沉积(DC Arc P lasm a Jet CVD)设备上,采用Ar-H2-CH4混合气体,通过调节甲烷浓度以及控制其他沉积参数,在Mo衬底上沉积出微/纳米复合自支撑金刚石膜。实验表明,当微米金刚石膜层沉积结束后,在随后... 在30kW级直流电弧等离子体喷射化学气相沉积(DC Arc P lasm a Jet CVD)设备上,采用Ar-H2-CH4混合气体,通过调节甲烷浓度以及控制其他沉积参数,在Mo衬底上沉积出微/纳米复合自支撑金刚石膜。实验表明,当微米金刚石膜层沉积结束后,在随后的沉积中,随着甲烷浓度的增加,金刚石膜表面的晶粒大小是逐渐减小的。当甲烷浓度达到20%以上时,金刚石膜生长面晶粒呈现菜花状的小晶团,膜体侧面已经没有了粗大的柱状晶,而是呈现出光滑的断口,对该层进行拉曼谱分析显示,位于1145 cm-1附近有一定强度的散射峰出现。这说明所沉积的晶粒全部变为纳米级尺寸。 展开更多
关键词 直流电弧等离子体喷射化学气相沉积 微/纳米复合自支撑金刚石膜 二次形核 拉曼光谱
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医用射流速度对生物组织破裂变形的影响规律
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作者 曾栋坪 罗林星 +2 位作者 唐正 王维 李佳敏 《振动与冲击》 北大核心 2026年第2期106-114,共9页
无针注射是先进给药技术发展的重要方向,注射试验难以直接获取医用射流与生物组织之间的相互作用力。采用光滑粒子流体动力学与有限元法,开展了射流注射在穿透阶段中医用水射流与多层生物组织之间的相互作用特性研究。通过对比射流穿透... 无针注射是先进给药技术发展的重要方向,注射试验难以直接获取医用射流与生物组织之间的相互作用力。采用光滑粒子流体动力学与有限元法,开展了射流注射在穿透阶段中医用水射流与多层生物组织之间的相互作用特性研究。通过对比射流穿透单层皮肤数值仿真与凝胶注射试验结果,验证数值仿真模型的可靠性,进而开展不同射流速度下医用水射流穿透多层生物组织仿真分析。研究结果表明:射流速度直接影响生物组织发生弹性变形及结构破坏,该生物组织模型的射流速度阈值为105 m/s,当射流速度由110 m/s增至120 m/s,脂肪层径向形变峰值由0.18 mm增至0.26 mm;同时,当射流速度由105 m/s增至120 m/s时,动能耗散速率增长了31%,即生物组织的动态力学响应会对射流产生明显的约束效应和运动阻滞作用,直接影响穿透过程中射流能量耗散特征。因此,注射过程中高速微射流与生物组织之间的耦合作用直接决定所形成孔洞的深度特征,可采用对数增长拟合模型对不同射流速度下的孔洞深度进行预测。 展开更多
关键词 无针注射 医用射流技术 射流速度 组织变形特征 光滑粒子流体动力学与有限元法
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Preparation and Characterization of High Quality Diamond Films by DC ArcPlasma Jet CVD Method 被引量:1
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作者 Guofang Zhong Fazheng Shen +1 位作者 Fanxiu Lu Weizhong Tang(Material Science and Engineering School, University of Science and Technology’ Beijing, Beijing 100083, China) 《International Journal of Minerals,Metallurgy and Materials》 SCIE EI CAS CSCD 1999年第4期281-284,共4页
Under optimal conditions free-standing high quality diamond films were prepared by DC arc plasma jet CVD method at a growth rate of 7-10 Pm/h. Surface and cross section morphologies of the diamond films were observed ... Under optimal conditions free-standing high quality diamond films were prepared by DC arc plasma jet CVD method at a growth rate of 7-10 Pm/h. Surface and cross section morphologies of the diamond films were observed by SEM. Raman spectrometer wasused to characterize the quality of diamond films. The IR transmittivity measured by IR spectrometer is close to the theoretical value ofabout 71% in the far infrared band. The thermal conductivity measured by photothermal deflection exceeds 18 W/cm' K. <l 10> is thepreferential growth orientation of the films detected by X-ray diffractometer. As s result, the extremely high temperature of DC arc plasma jet can produce supersaturated atomic hydrogen, which played an important role in the process for the deposition of high quality diamond films. 展开更多
关键词 D.C. plasma jet CVD diamond films free-standing CHARACTERIZATION
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Theoretical Mechanism Analysis of 3D Free Surface Electrospinning
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作者 邓宗良 魏亮 +2 位作者 梁志勇 覃小红 周逸竹 《Journal of Donghua University(English Edition)》 EI CAS 2017年第4期518-522,共5页
Electrospinning is a new type of free-end spinning built on the electric field. The electric force of polyacrylonitrile( PAN)polymer solution overcomes the surface tension of the solution,and then it causes wave and f... Electrospinning is a new type of free-end spinning built on the electric field. The electric force of polyacrylonitrile( PAN)polymer solution overcomes the surface tension of the solution,and then it causes wave and forms jet flow. In the process of injection,the solution is evaporated or solidified,eventually forming a fiber on the receiving device. Different from ordinary single needle head,in the study,a new type of 3D free surface spinneret is used to produce multiple jets at the same time, and this will greatly improve production efficiency. In the paper,the model of 3D free surface is analyzed by the theory of fluid mechanics. The relationship among the wave length,surface tension and the electric field is obtained.After the mechanical analysis on the stable period of the jet,the relationship between the jet radius and the distance from the spinneret to jet is carried out. At the same time the relationship between the jet velocity and the tensile force is carried out. After mechanics analyzing on the unstable period of the jet,it can be concluded that the radius of the jet is inversely proportional to one half power of the distance from the jet to the spinneret,and the electrostatic spinning jet's velocity is directly proportional to one half power of the tensile force. After the mechanical analysis of the unstable period of the electrospinning jet,it can be concluded that the radius of the jet is inversely proportional to one fourth power of the jet intercept point distance. 展开更多
关键词 ELECTROSPINNING free surface surface tension WAVELENGTH jet
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Design and Numerical Simulation of Low-Fiber Hollow Spindle in Air-Jet Vortex Spinning 被引量:1
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作者 张肖斌 薛文良 程隆棣 《Journal of Donghua University(English Edition)》 EI CAS 2015年第1期119-124,共6页
Based on the mechanical system of free-end fibers and the analysis of pulling free-end fibers out of the spun yarn during spinning,a low-fiber hollow spindle is designed and the air distribution of fluent field is sim... Based on the mechanical system of free-end fibers and the analysis of pulling free-end fibers out of the spun yarn during spinning,a low-fiber hollow spindle is designed and the air distribution of fluent field is simulated numerically. The negative pressure effect is much bigger at the top of low-fiber hollow spindle than that in Murata No.861,which is more conducive for single fiber to get into the channel of hollow spindle. The tangential velocity in 0-3 mm at the top of hollow spindle increases and the fluctuation of radial velocity is much stronger,which enhance the wrapping effect. In the addition,the distribution of axial velocity remains the same. 展开更多
关键词 air-jet vortex spinning numerical simulation free-end fiber mechanical system low-fiber hollow spindle
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同济气动声学风洞声场品质测试
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作者 庞加斌 刘劲松 +2 位作者 邢鹏 李泽 李田田 《同济大学学报(自然科学版)》 北大核心 2025年第9期1457-1461,1470,共6页
气动声学风洞的声场品质包括试验段驻室自由声场、背景噪声和低频压力脉动3个方面指标。同济气动声学风洞声场测试结果显示,160 km·h^(-1)风速的背景噪声A计权总声压级为61 dB(A),50~200 km·h^(-1)风速范围内的低频压力脉动... 气动声学风洞的声场品质包括试验段驻室自由声场、背景噪声和低频压力脉动3个方面指标。同济气动声学风洞声场测试结果显示,160 km·h^(-1)风速的背景噪声A计权总声压级为61 dB(A),50~200 km·h^(-1)风速范围内的低频压力脉动系数小于0.5%;滚动路面系统的移动带抽吸在80 km·h^(-1)风速以下干扰背景噪声,但对低频压力脉动没有影响;按照ISO 3745∶2012标准,试验段驻室自由声场截止频率低至50 Hz,且63 Hz及以上自由声场半径达到9 m。 展开更多
关键词 气动声学风洞 自由射流剪切层 背景噪声 低频压力脉动 滚动路面系统
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The Effects of Gas Composition on the Atmospheric Pressure Plasma Jet Modification of Polyethylene Films
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作者 孙洁 邱夷平 《Plasma Science and Technology》 SCIE EI CAS CSCD 2015年第5期402-408,共7页
Polyethylene (PE) films are treated using an atmospheric pressure plasma jet (APPJ) with He or He/O2 gas for different periods of time. The influence of gas type on the plasma polymer interactions is studied. The ... Polyethylene (PE) films are treated using an atmospheric pressure plasma jet (APPJ) with He or He/O2 gas for different periods of time. The influence of gas type on the plasma polymer interactions is studied. The surface contact angle of the PE film can be effectively lowered to 58° after 20 s of He/O2 plasma treatment and then remains almost unchanged for longer treatment durations, while, for He plasma treatment, the film surface contact angle drops gradually to 47° when the time reaches 120 s. Atomic force microscopy (AFM) results show that the root mean square (RMS) roughness was significantly higher for the He/O2 plasma treated samples than for the He plasma treated counterparts, and the surface topography of the He/O2 plasma treated PE films displays evenly distributed dome-shaped small protuberances. Chemical composition analysis reveals that the He plasma treated samples have a higher oxygen content but a clearly lower percentage of COO than the comparable He/O2 treated samples, suggesting that differences exist in the mode of incorporating oxygen between the two gas condition plasma treatments. Electron spin resonance (ESR) results show that the free radical concentrations of the He plasma treated samples were clearly higher than those of the He/O2 plasma treated ones with other conditions unchanged. 展开更多
关键词 atmospheric pressure plasma jet PE film WETTABILITY free radicals plasma- polymer interactions
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三喷嘴开放式撞击流反应器液滴破碎行为可视化实验研究
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作者 张珺 梁鹏飞 刘有智 《化学工程》 北大核心 2025年第10期55-61,共7页
采用高速相机对三喷嘴开放式撞击流反应器内不同入射速度、水平喷嘴间距w以及垂直喷嘴间距h下液滴破碎过程、直径、速度等液滴行为进行研究。入射速度增大,液滴拉伸断裂越早,越容易形成液滴,液滴数量显著增大,液滴直径概率密度峰值左移... 采用高速相机对三喷嘴开放式撞击流反应器内不同入射速度、水平喷嘴间距w以及垂直喷嘴间距h下液滴破碎过程、直径、速度等液滴行为进行研究。入射速度增大,液滴拉伸断裂越早,越容易形成液滴,液滴数量显著增大,液滴直径概率密度峰值左移,液滴直径减小,液滴分布更窄、更均匀,径向速度u和轴向速度v均增大。但同时增大w、h,液滴直径增大,液滴直径概率密度峰值右移;由于液滴尺寸、入射速度及喷嘴间距的影响,液滴向y轴负方向运动时,u和v变化规律不一致。研究结果表明:较小入射速度下,喷嘴间距对液滴破碎影响较显著,随入射速度增大,入射速度和喷嘴间距对液滴破碎影响更加复杂。 展开更多
关键词 三喷嘴开放式撞击流 液滴直径 径向速度 轴向速度 液滴破碎
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发动机高空模拟中引射器的气动设计
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作者 张海栋 冯欣 戴芳立 《机电产品开发与创新》 2025年第3期6-8,共3页
简要介绍了发动机自由射流式高空模拟用排气引射系统的组成和工作原理,针对某发动机模拟高度25km以下、飞行马赫数4以下自由射流高空模拟试验的典型工况和对排气环境压力的需求,给出了关键部件引射器的结构形式,开展了引射器的设计计算... 简要介绍了发动机自由射流式高空模拟用排气引射系统的组成和工作原理,针对某发动机模拟高度25km以下、飞行马赫数4以下自由射流高空模拟试验的典型工况和对排气环境压力的需求,给出了关键部件引射器的结构形式,开展了引射器的设计计算和仿真分析。结果表明,采用两级串联中心引射结构在给定的蒸汽作用下满足额定负载45kg/s,典型发动机自由射流试验工况25km的引射能力要求,验证了此引射方案的可行性。 展开更多
关键词 发动机高空模拟 自由射流 排气引射系统 气动计算 数值分析
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流向磁场下液态金属射流破碎特性的实验研究
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作者 李扬 陈龙 +1 位作者 阳倦成 吕泽 《中国科学院大学学报(中英文)》 北大核心 2025年第4期433-440,共8页
为深入理解液态金属射流的磁流体力学特性,基于自行搭建的液态金属射流实验平台,对流向磁场条件下液态金属镓铟锡射流破碎过程开展实验研究。从射流形态、破碎长度、表面扰动和液滴分布4个方面分析射流破碎特性。无磁场时破碎长度随We... 为深入理解液态金属射流的磁流体力学特性,基于自行搭建的液态金属射流实验平台,对流向磁场条件下液态金属镓铟锡射流破碎过程开展实验研究。从射流形态、破碎长度、表面扰动和液滴分布4个方面分析射流破碎特性。无磁场时破碎长度随We增大而增大,射流表面波长在表面张力的作用下趋近于临界波长,射流破碎液滴体积直径呈现双峰结构。施加流向磁场后,射流破碎形成的液滴发生振动衰减,在破碎位置下游呈现等大球形液滴,表面波长随磁场的增强而变短,射流破碎长度随磁场的增强而变长。最后归纳了流向磁场对射流破碎长度的3种影响方式。 展开更多
关键词 液态金属 自由射流 破碎特性 流向磁场
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