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基于Fluent角型喷嘴内部空化行为的数值模拟 被引量:9
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作者 赵丁选 王倩 杜苗苗 《东北大学学报(自然科学版)》 EI CAS CSCD 北大核心 2016年第9期1283-1287,共5页
利用Fluent流体计算软件对角型喷嘴内部的空化流场进行了数值模拟,得到了喷嘴内部的压力、气相生成速率和汽含率分布场,并对三种扩张角喷嘴内的流场进行了比较分析.结果表明:在角型喷嘴内部,空化汽泡主要在喷嘴圆柱段壁面起始点和扩张... 利用Fluent流体计算软件对角型喷嘴内部的空化流场进行了数值模拟,得到了喷嘴内部的压力、气相生成速率和汽含率分布场,并对三种扩张角喷嘴内的流场进行了比较分析.结果表明:在角型喷嘴内部,空化汽泡主要在喷嘴圆柱段壁面起始点和扩张段壁面起始点两处产生;在扩张段壁面起始点处,由于回流和压力两种因素的共同作用导致扩张角对空化汽泡生成速率的影响存在最优值;随着扩张角的减小,角型喷嘴在扩张段壁面的空化区域不断扩大,其汽含率也不断攀升;扩张角的改变对角型喷嘴圆柱段区域的空化行为没有明显影响. 展开更多
关键词 空化 角型喷嘴 扩张 数值模拟 汽含率
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空化射流角型喷嘴内流场的数值模拟 被引量:16
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作者 管金发 邓松圣 +1 位作者 郭广东 华卫星 《机床与液压》 北大核心 2012年第23期46-50,共5页
建立了角型喷嘴物理模型。基于FLUENT软件,采用混合模型、空化模型和RNG k-ε紊流模型对空化射流喷嘴内流场进行数值模拟。以径向线上蒸汽体积分数分布、轴线上蒸汽体积分数分布和速度分布为判断角型喷嘴产生的空化射流空化程度的依据,... 建立了角型喷嘴物理模型。基于FLUENT软件,采用混合模型、空化模型和RNG k-ε紊流模型对空化射流喷嘴内流场进行数值模拟。以径向线上蒸汽体积分数分布、轴线上蒸汽体积分数分布和速度分布为判断角型喷嘴产生的空化射流空化程度的依据,分析圆柱段直径、入口压力、出口压力对射流空化程度的影响规律。模拟结果表明:圆柱段直径的最佳初始值为1 mm;增大入口压力可以提高射流空化程度,但随着出口压力的增大,又会抑制喷嘴内空化的初生并降低出口速度,不利于射流空化程度的提高。 展开更多
关键词 空化射流 角型喷嘴 空化程度 数值模拟
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The Effect of Diffuser Angle on the Discharge Coefficient of a Miniature Critical Nozzle 被引量:5
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作者 Jae Hyung Kim Heuy Dong Kim Toshiaki Setoguchi 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第3期222-227,共6页
Many researches on critical nozzles have been performed to accurately measure the mass flow rate of gas flow,and to standardize the performance as a flow meter.Recently,much interest is being paid on the measurement o... Many researches on critical nozzles have been performed to accurately measure the mass flow rate of gas flow,and to standardize the performance as a flow meter.Recently,much interest is being paid on the measurement of very small mass flow rate in industry fields such as MEMS applications.However,the design and performance data of the critical nozzles obtained so far have been applied mainly to the critical nozzles with comparatively large diameters,and the works available on miniature critical nozzles are lacking.In the present study,a computational fluid dynamics method has been applied to investigate the influence of the diffuser angle on discharge coefficient of the miniature critical nozzles.In computations,the throat diameter of critical nozzle is varied from 0.2 mm to 5.0 mm and the diffuser angle is changed from 2 deg to 8 deg.The computational results are validated with some experimental data available.The results show that the present computational results predict appropriately the discharge coefficient of the gas flows through miniature critical nozzles.It is known that the discharge coefficient is considerably influenced by the diffuser angle,as the throat diameter of nozzle becomes small below a certain value.This implies that the miniature critical nozzles should be carefully designed. 展开更多
关键词 Compressible Flow Critical Nozzle Compressible Flow Discharge Coefficient Diffuser Configuration Reynolds Number
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