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NASA低速离心压气机叶轮内部流动的数值研究
引用本文:席光,王晓锋,樊会元,倪明玖.NASA低速离心压气机叶轮内部流动的数值研究[J].工程热物理学报,2001,22(2):188-191.
作者姓名:席光  王晓锋  樊会元  倪明玖
作者单位:西安交通大学能动学院,
基金项目:教育部高校骨干教师资助计划,1998[9],
摘    要:本文采用一多功能流体动力学计算软件,详细计算分析了NASA低速离心压气机叶轮内部的三维速度场。通过与实验数据以及其它软件计算结果详细定量的对比分析,研究了CFD软件预测叶轮内部流场的能力及存在的问题,提出了进一步提高数值计算精度的建议。

关 键 词:数值分析  离以压气机  变工况
文章编号:0253-231X(2001)02-0188-04
修稿时间:2000年12月12

NUMERICLE STUDY OF THE FLOW INSIDE THE NASA 'S LOW-SPEED CENTRIFUGAL COMPRESSOR IMPELLER
Xi Guang,WANG Xiao-Feng,FAN Hui-Yuan,NI Ming-Jiu.NUMERICLE STUDY OF THE FLOW INSIDE THE NASA 'S LOW-SPEED CENTRIFUGAL COMPRESSOR IMPELLER[J].Journal of Engineering Thermophysics,2001,22(2):188-191.
Authors:Xi Guang  WANG Xiao-Feng  FAN Hui-Yuan  NI Ming-Jiu
Abstract:Based on a multifunctional CFD software, thethree-dimensional velocity field within the impeller of NASA low-speed centrifugal compressor is computed in detail in this paper.Detailed quantitative analysis is then carried out through comparing the results with experimental data as well as the results from another CFD software. Moreover, the ability of CFD sof ware to predict the flow field inside the impeller and the existing problems are studied. Suggestions are given to further improve numerical computation precision.
Keywords:numerical analysis  centrifugal compressor  and non-design working condition
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