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Investigations on an Axial Flow Fan Stage subjected to Circumferential Inlet Flow Distortion and Swirl 被引量:20
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作者 M. Govardhan K. Viswanath (Thermal Turbomachines Laboratory Department of Mechanical Engineering, Indian Institute of Technology, Madras 600 036, India ) 《Journal of Thermal Science》 SCIE EI CAS CSCD 1997年第4期241-250,共10页
The combined effects of swirl and circumferential inlet flow distortion on the flow field of an axial flow fan stage are reported in this paper. The study involves measurements at the inlet of the rotor and exit of th... The combined effects of swirl and circumferential inlet flow distortion on the flow field of an axial flow fan stage are reported in this paper. The study involves measurements at the inlet of the rotor and exit of the rotor and stator at design and off design now conditions. The study indicated that at the design flow condition, swirl had caused deterioration of the performance in addition to that caused by distortfou. Pressure rise imparted in the distortion zone is higher than in the free zone. The attenuation of distortion is high in the presence of swirl. 展开更多
关键词 circumferential distortion swirl inlet guide vanes distortion index
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旋流对同轴富氧扩散燃烧NOx排放的影响 被引量:16
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作者 赵黛青 杨浩林 杨卫斌 《燃烧科学与技术》 EI CAS CSCD 北大核心 2008年第5期383-387,共5页
对30%-40%的氧浓度下甲烷富氧空气同轴扩散燃烧的火焰形态、可见火焰高度、燃烧特性以及NOx排放进行了实验测量,研究了旋流数对NOx排放控制的影响.结果显示,随着旋流数的增加,火焰高度略有升高,火焰发光由白色逐渐变为橙黄色;... 对30%-40%的氧浓度下甲烷富氧空气同轴扩散燃烧的火焰形态、可见火焰高度、燃烧特性以及NOx排放进行了实验测量,研究了旋流数对NOx排放控制的影响.结果显示,随着旋流数的增加,火焰高度略有升高,火焰发光由白色逐渐变为橙黄色;最高火焰温度逐渐降低,温度分布也变得平坦;NOx排放指数随旋流数的增加而降低,氧浓度越高,其下降幅度越大.保持其他条件不变,增加氧化剂流速可以增强旋流对燃烧特性及NOx排放的影响. 展开更多
关键词 富氧燃烧 旋流 扩散火焰 NOx
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进气道旋流模拟及测量的风洞试验研究 被引量:13
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作者 邓小宝 姜健 +2 位作者 屈霁云 张堃元 叶飞 《燃气涡轮试验与研究》 2009年第4期51-56,共6页
利用设计的叶片式旋流发生器,在某小型低速风洞中进行了整体涡旋流、局部涡旋流、对涡旋流的模拟,对三孔探针、五孔探针进行了标定,对所模拟出的旋流进行了测量。风洞试验结果表明:发动机进口前2倍直径处安装旋流发生器可保证旋流的强... 利用设计的叶片式旋流发生器,在某小型低速风洞中进行了整体涡旋流、局部涡旋流、对涡旋流的模拟,对三孔探针、五孔探针进行了标定,对所模拟出的旋流进行了测量。风洞试验结果表明:发动机进口前2倍直径处安装旋流发生器可保证旋流的强度最大;设计的旋流发生器可产生28°的整体涡旋流;旋流发生器叶片攻角对旋流强弱的影响较为明显;不同叶片布局方式可得到不同形式的旋流流场;旋流的诱导速度对旋流中心位置有较大的影响;三孔探针用于测量旋流时受径向偏转气流的影响,时有不稳定现象。 展开更多
关键词 进气道 旋流 旋流发生器 三孔探针 五孔探针 风洞试验
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S形进气道和发动机相容性 被引量:14
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作者 杨国才 《推进技术》 EI CAS CSCD 北大核心 1995年第6期26-29,共4页
进气道旋流是进/发相容性的一个重大扰动参数。在发动机稳定性和性能方面进气道旋流的效应也是不可忽视的。讨论了S形进气道/发动机相容性的评定方法,并且建议了有效评定准则。S形进气道/发动机相容性评定必须由两部分组成,一部... 进气道旋流是进/发相容性的一个重大扰动参数。在发动机稳定性和性能方面进气道旋流的效应也是不可忽视的。讨论了S形进气道/发动机相容性的评定方法,并且建议了有效评定准则。S形进气道/发动机相容性评定必须由两部分组成,一部分与压力畸变有关,而另一部分与流动弯曲度有关。 展开更多
关键词 进气道 旋涡 流场 相容性 航空发动机
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Experimental investigations of the spray structure and interactions between sectors of a double-swirl low-emission combustor 被引量:11
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作者 Xiongjie FAN Cunxi LIU +3 位作者 Gang XU Chi ZHANG Jianchen WANG Yuzhen LIN 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2020年第2期589-597,共9页
In this paper,the spray characteristics of a double-swirl low-emission combustor are analyzed by using Particle Imaging Velocimetry(PIV)and Planar Laser Induced Fluorescence(PLIF)technologies in an optical three-secto... In this paper,the spray characteristics of a double-swirl low-emission combustor are analyzed by using Particle Imaging Velocimetry(PIV)and Planar Laser Induced Fluorescence(PLIF)technologies in an optical three-sector combustor test rig.Interactions between sectors and the influence of main stage swirl intensity on spray structure are explained.The results illustrate that the swirl intensity has great effect on the flow field and spray structure.The spray cone angle is bigger when the swirl number is 0.7,0.9 than that when the swirl number is 0.5.The fuel distribution zone is larger and the distribution is more uniform when the swirl number is 0.5.The fuel concentration in the center area of the center plane of side sector(Plane 5)is larger than that of the center plane of middle sector(Plane 1).The spray cone angle in Plane 5 is larger than that in Plane 1.The width of spray cone becomes larger with the increase of Fuel-Air Ratio(FAR),whereas the spray cone angle under different fuel-air ratios are absolutely the same.The results of the mechanism of spray organization in this study can be used to support the design of new low-emission combustor. 展开更多
关键词 COMBUSTOR Fuel-air ratio PIV PLIF Pressure DROP swirl intensity
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一种“全可控涡”三元叶轮设计叶片涡的给定方法 被引量:10
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作者 张莉 陈汉平 徐忠 《流体机械》 CSCD 北大核心 2000年第8期14-17,共4页
针对“全可控涡”三元叶轮设计方法中叶片涡的给定环节 ,在考虑气动力学条件的基础上 ,介绍了一种确定叶片涡在子午流面分布的数学模型 ,编制了计算机程序 ,提供了一种快速确定子午流面叶片涡分布的方法。
关键词 离心叶轮 叶片涡 设计 全可控涡 双调和方程
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Effects of Inlet Swirl on the Flow in a Steam Turbine Exhaust Hood 被引量:12
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作者 MiroslavStastny LadislavTajc 《Journal of Thermal Science》 SCIE EI CAS CSCD 2000年第4期327-333,共7页
The flow in the exhaust hood of a condensing steam turbine depends to a considerable extent on the inlet swirl of the flow which changes in tandem with the volumetric flow of steam through the last stage. This study g... The flow in the exhaust hood of a condensing steam turbine depends to a considerable extent on the inlet swirl of the flow which changes in tandem with the volumetric flow of steam through the last stage. This study gives a description of experiments which were carried out on the exhaust hood of a 500 MW steam turbine under various conditions, e.g. when there is rated power, when there is an idle run, or when there are various pressures in the condenser. The flow in a model exhaust hood was investigated by means of CFD methods. Computations were performed with the help of the FLUENT 5 code which is based on solving the Navier-Stokes equations while taking the RSM and LES models of turbulence into consideration. The results of the computations are in full conformity with the experiments. 展开更多
关键词 swirl of the now steam turbine exhaust hood now separation turbulence model.
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Heat Transfer and Friction Factor Studies in a Circular Tube Fitted with Twisted Tape Consisting of Wire-nails 被引量:13
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作者 P. Murugesan K. Mayilsamy S. Suresh 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2010年第6期1038-1042,共5页
This paper deals with the experimental investigation on Nusselt number,friction factor and thermal en-hancement factor of a double pipe heat exchanger equipped with twisted tape consisting wire nails(WN-TT) and plain ... This paper deals with the experimental investigation on Nusselt number,friction factor and thermal en-hancement factor of a double pipe heat exchanger equipped with twisted tape consisting wire nails(WN-TT) and plain twisted tapes(P-TT) with three different twist ratios of y 2.0,4.4 and 6.0. Test runs are conducted using the water as the working fluid with Reynolds number range between 2000 and 12000 for WN-TT and P-TT. It is found that Nusselt number,friction factor and thermal enhancement factor in the tube equipped with WN-TT appreciably higher than those in the tube fitted with P-TT and plain tube. Over the range considered Nusselt number,friction factor and thermal enhancement factor in a tube with WN-TT are respectively,1.08 to 1.31,1.1 to 1.75 and 1.05 to 1.13 times of those in tube with P-TT. The better performance of WN-TT is due to combined effects of the follow-ing factors:(1) common swirling flow generated by P-TT,(2) additional turbulence offered by the wire nails. Em-pirical correlations for Nusselt number,friction factor and thermal enhancement factor are also formulated from the experimental results of WN-TT and P-TT. 展开更多
关键词 heat transfer enhancement friction factor plain twisted tape TURBULENCE swirl flow
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不同结构消声器内部流场的比较 被引量:12
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作者 王伟 李国祥 +2 位作者 倪计民 肖国权 田永祥 《内燃机学报》 EI CAS CSCD 北大核心 2007年第3期277-280,共4页
通过对两种不同结构消声器内部流场的模拟,研究了气流对消声器的影响。以两种典型消声器I和消声器II为例,对内部流场进行对比分析。消声器结构不同,内部产生的涡流也不同,气流经过消声器I的内插管后,进入第二腔产生两处大的涡流,而消声... 通过对两种不同结构消声器内部流场的模拟,研究了气流对消声器的影响。以两种典型消声器I和消声器II为例,对内部流场进行对比分析。消声器结构不同,内部产生的涡流也不同,气流经过消声器I的内插管后,进入第二腔产生两处大的涡流,而消声器II有4处大的涡流,强度也比消声器I的大。模拟计算出的入口绝对压力可以作为设计优化消声器结构流动阻力大小的依据。消声器尾管采用穿孔管,可以对消声器再生噪声在出口处进行衰减,但同时也增加了流动阻力。 展开更多
关键词 消声器 数值模拟 流场 绝对压力 涡流
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在进气道与发动机相容性方面反旋流措施的工程应用研究 被引量:12
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作者 杨国才 《推进技术》 EI CAS CSCD 北大核心 1995年第4期28-33,共6页
进气道旋流(Intakswirl)是进气道与发动机相容性的一个重大扰动参数。从飞机总体布局、发动机设计方面入手,研究了现存飞机对旋流的防止和反抗措施。新发现:低压压气机前面级静子叶片采取“端弯”技术措施,对提高发动机... 进气道旋流(Intakswirl)是进气道与发动机相容性的一个重大扰动参数。从飞机总体布局、发动机设计方面入手,研究了现存飞机对旋流的防止和反抗措施。新发现:低压压气机前面级静子叶片采取“端弯”技术措施,对提高发动机抗旋流扰动能力,降低对旋流扰动的敏感度十分有利,看好其工程应用前景。 展开更多
关键词 航空发动机 进气道 旋涡 匹配
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S弯进气道内旋流的有源涡控研究 被引量:6
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作者 林麒 郭荣伟 《航空学报》 EI CAS CSCD 北大核心 1989年第1期A35-A40,共6页
本文给出了来流攻角为30°和40°、进口带分离区的方转圆截面S弯扩压管道内进行抽气形式的有源涡控的气流特性。研究表明,随涡控抽气量增加,旋流明显减小,当抽气量足够大时,整体涡基本被消除;出口平均总压损失下降;总压畸变减小... 本文给出了来流攻角为30°和40°、进口带分离区的方转圆截面S弯扩压管道内进行抽气形式的有源涡控的气流特性。研究表明,随涡控抽气量增加,旋流明显减小,当抽气量足够大时,整体涡基本被消除;出口平均总压损失下降;总压畸变减小;管道出口流量增大。因此,抽气形式的有源涡控是抑制旋流、减少出口总压平均损失、改善S弯进气道出口流场的有效措施。 展开更多
关键词 扩压器 旋流 涡控 进气道
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Periodic atomization characteristics of simplex swirl injector induced by klystron effect 被引量:10
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作者 Anlong YANG Shangrong YANG +1 位作者 Yunfei XU Longfei LI 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2018年第5期1066-1074,共9页
The atomization dynamic characteristics of a simplex swirl injector was investigated experimentally by using a hydrodynamic mechanical pulsator and the shadow photography technique. The frequency response characterist... The atomization dynamic characteristics of a simplex swirl injector was investigated experimentally by using a hydrodynamic mechanical pulsator and the shadow photography technique. The frequency response characteristics of the fluid film and atomization fluctuations and their correlations with pressure fluctuations were obtained by using an in-house code of image processing. It is demonstrated that the klystron effect induced by periodic pressure fluctuations results in periodic liquid film fluctuation with large amplitudes, periodic superposition of droplets and reduction of the breakup length. It was found that the atomization of the simplex swirl injector only responds to the pressure fluctuation in frequency range approximately from 0 to 300 Hz, and it is particularly sensitive to pressure fluctuations at frequencies from 100 to 200 Hz. According to this experiment, the responsive frequency limitation is merely affected by injector configuration, rather than the supply line. 展开更多
关键词 ATOMIZATION Combustion stability Klystron effect Liquid rocket engine Simplex swirl injector
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Compound Heat Transfer Enhancement of a Converging-Diverging Tube with Evenly Spaced Twisted-tapes 被引量:12
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作者 洪蒙纳 邓先和 +1 位作者 黄阔 李志武 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2007年第6期814-820,共7页
Pressure drop and compound heat transfer characteristics of a converging-diverging tube with evenly spaced twisted-tapes (CD-T tube) have been investigated experimentally. Swirl was generated by evenly spaced twiste... Pressure drop and compound heat transfer characteristics of a converging-diverging tube with evenly spaced twisted-tapes (CD-T tube) have been investigated experimentally. Swirl was generated by evenly spaced twisted-tape elements which vary in twist ratio and rotation angle. Space ratio also has an important effect on the characteristics. For comparison, experiments in a smooth circular tube and a converging-diverging (CD) tube with-out twisted-tapes were carried out. The results show that the twisted-tape with twist ratio y=4.72 and rotation angle θ=180° has the best performance among the four types of twisted-tapes presented in this paper. At Reynolds number ranging from 3400 to 20000, when space ratio s=48.6, the heat transfer efficiency index, which increases as the Reynolds number increases, is 0.85-1.21 and 1.07-1.15 compared to that of a smooth circular tube and a CD tube without twisted-tape inserts, respectively. 展开更多
关键词 compound heat transfer spaced-twisted-tape converging-diverging tube swirl flow
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单位熵产分析法在强化传热研究中的应用 被引量:11
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作者 高翔 骆仲泱 +2 位作者 周劲松 倪明江 岑可法 《化工学报》 EI CAS CSCD 北大核心 1998年第5期639-643,共5页
Based on the second law or the rmodynamics,the authors proposed the unit entropy generation analysis method for evaluation and analysis of the comprehensive thermal characteristics of different enhanced heat transfer ... Based on the second law or the rmodynamics,the authors proposed the unit entropy generation analysis method for evaluation and analysis of the comprehensive thermal characteristics of different enhanced heat transfer methods.The optimum operation condition of the enhanced heat transfer methods,such as fin type and swirl flow,is obtained through thermal characteristic analysis.This work provides a theoretical basis for engineering design. 展开更多
关键词 强化传热 单位熵产分析法 肋片 旋流 传热
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S弯进气道旋流研究 被引量:10
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作者 杨国才 郑遂 《推进技术》 EI CAS CSCD 北大核心 1992年第1期1-7,共7页
根据理论分析,更主要的是根据实验结果,证明了某S弯常规超音速腹部进气道对侧滑敏感,并产生整涡旋流,它取决于进口没有导向叶片发动机对旋流扰动的敏感程度。发动机,性能下降,发动机喘振和强迫叶片振动之类严重的进气道与发动机匹配问... 根据理论分析,更主要的是根据实验结果,证明了某S弯常规超音速腹部进气道对侧滑敏感,并产生整涡旋流,它取决于进口没有导向叶片发动机对旋流扰动的敏感程度。发动机,性能下降,发动机喘振和强迫叶片振动之类严重的进气道与发动机匹配问题可能出现。 对用动态总压畸变作为主要相容性参数提出了疑问,认为旋流是进气道与失速裕度较大发动机匹配的决定性的相容性参数。 新发现一种不测量旋流也可以快速地判断进气道出口是否存在有整涡旋流的方法。 展开更多
关键词 进气道 旋涡 研究 航空发动机
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WEAKLY SWIRLING TURBULENT FLOW IN TURBID WATER HYDRAULIC SEPARATION DEVICE 被引量:9
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作者 LI Lin QIU Xiu-yun +2 位作者 JIN Sheng XIAO Jun GONG Shou-yuan 《Journal of Hydrodynamics》 SCIE EI CSCD 2008年第3期347-355,共9页
This article deals with the characteristics of weakly swirling turbulent flow field in a Turbid Water Hydraulic Separation Device (TWHSD) through experimental and numerical researches. The flow field was measured by... This article deals with the characteristics of weakly swirling turbulent flow field in a Turbid Water Hydraulic Separation Device (TWHSD) through experimental and numerical researches. The flow field was measured by PIV, which provided streamlines, vortex structure, vorticity and velocity distribution in different test planes in the TWHSD. On the basis of the experimental results, the tangential and radial velocity distributions of the swirling flow field were obtained. Meanwhile, the numerical simulations were conducted with the RNG κ-ε and RSM turbulence models, respectively. According to the experimental and numerical results, the characteristics of the clear water flow field inside the TWHSD were determined. In view of simulation accuracy and time consumption, it is suggested to apply the RNG κ-ε model instead of the RSM model, which is more time consuming, to make further study on two-phases flow fields in the device. 展开更多
关键词 hydraulic turbid water separation device weak swirl flow field Computational Fluid Dynamics(CFD) turbulence models
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燃烧室形状对105型柴油机缸内气体流动和排放特性的影响 被引量:3
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作者 段树林 吕林 +2 位作者 肖进 吴锦翔 高孝洪 《农业机械学报》 EI CAS CSCD 北大核心 2000年第4期14-17,共4页
分析了燃烧室形状对柴油机缸内气体流动和排放特性的影响。用三维有限元程序 ,在不喷射燃油的情况下 ,系统地分析了缸内气体涡流、挤流、湍流动能等参数随曲轴转角的变化关系 ,并在单缸 1 0 5型柴油机上进行了性能试验。计算和试验结果... 分析了燃烧室形状对柴油机缸内气体流动和排放特性的影响。用三维有限元程序 ,在不喷射燃油的情况下 ,系统地分析了缸内气体涡流、挤流、湍流动能等参数随曲轴转角的变化关系 ,并在单缸 1 0 5型柴油机上进行了性能试验。计算和试验结果表明 ,优化燃烧室几何形状可以延长缸内高涡流的持续时间 ,活跃燃烧后期的扩散燃烧。通过延迟喷油定时 ,可以达到 NOx。 展开更多
关键词 柴油机 燃烧室形状 涡流 排放特性 气体流动
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A Parametric Study for High-Efficiency Gas-Liquid Separator Design 被引量:11
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作者 S.Nagdewe J.K.Kwoon +3 位作者 H.D.Kim D.S.Kim K.M.Kwak Toshiaki Setoguchi 《Journal of Thermal Science》 SCIE EI CAS CSCD 2008年第3期238-242,共5页
A gas liquid centrifugal separator is widely used in industry on account of its simple geometry and little maintenance. These separators have considerable advantages over filters, scrubbers or precipitators in term of... A gas liquid centrifugal separator is widely used in industry on account of its simple geometry and little maintenance. These separators have considerable advantages over filters, scrubbers or precipitators in term of compact design, lower pressure drop and higher capacity. A gas liquid centrifugal separator is a device that utilizes centrifugal forces and low pressure caused by rotational motion to separate liquid from gas by density differences. Efficient and reliable separation is required for the optimum operation. These separators are often operated at less than peak efficiency due to the entrainment of separated liquid through an outlet pipe which is closely associated with the very complicated flow phenomena involved. Design parameters such as length of the separation space, vane exit angle, inlet to outlet diameter ratio, models for separation efficiency and pressure drop as a function of physical dimensions are not available in literature. This leaves the designer with very little to go on except known designs and experimentation. The aim of present study is to perform a parametric study to get higher efficiency for gas-liquid separator. A parametric study has been carded out with the help of CFD tools to analyze a separation performance of a centrifugal separator by varying the length of separator space. The best design parameters are analyzed based upon obtained results, tangential velocities, vortices, total pressure losses. From the present study several attempts are made to improve the performance of conventional centrifugal separators. 展开更多
关键词 Centrifugal separator Gas-liquid two-phase flow swirl vane k-c RNG turbulence model Tangentialvelocity
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“可控涡”法设计离心叶轮的应用研究 被引量:6
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作者 李超 张瑞成 《动力工程》 CSCD 北大核心 2003年第6期2845-2849,共5页
详细介绍了用"可控涡"法设计离心叶轮时叶片涡给定的几种方法,通过编制程序确定了叶片涡rCu在子午流面上的分布。并利用确定的可控涡对一离心叶轮进行了反问题设计。计算结果表明:速度分布合理,满足设计要求。
关键词 叶轮 可控涡 三元流动 设计
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进口导流叶片对S弯进气道出口旋流的抑制研究 被引量:8
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作者 郭荣伟 梁德旺 陈贻忠 《空气动力学学报》 CSCD 北大核心 1996年第2期141-147,共7页
本文通过在S弯管道进口段安装水平导流叶片,引主流气流吹除进口分离,有效地抑制了出口旋流和流场压力畸变,使总压恢复提高。其抑制效果与叶片的安装角、安装位置及叶片宽度等参数有关。文中还探讨了安装多块导流叶片时的旋流抑制效... 本文通过在S弯管道进口段安装水平导流叶片,引主流气流吹除进口分离,有效地抑制了出口旋流和流场压力畸变,使总压恢复提高。其抑制效果与叶片的安装角、安装位置及叶片宽度等参数有关。文中还探讨了安装多块导流叶片时的旋流抑制效果。给果表明安装三块导流叶片可进一步降低族流,减小流场压力畸变,并可以彻底消除单涡旋流,且有总压恢复提高。 展开更多
关键词 进气道 导流叶片 流场畸变 涡流
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