首页 | 本学科首页   官方微博 | 高级检索  
     检索      

轴流压气机重复级边界条件的建立及其在流场数值诊断中的应用
引用本文:邹正平,徐力平,张志芳.轴流压气机重复级边界条件的建立及其在流场数值诊断中的应用[J].航空动力学报,2000,15(1):22-26.
作者姓名:邹正平  徐力平  张志芳
作者单位:北京航空航天大学404教研室!北京100083(邹正平,徐力平),沈阳航空发动机研究所!辽宁沈阳110015(张志芳)
摘    要:本文对轴流压气机多级环境中存在的重复级流动现象的建立及其在流场数值模拟中的应用进行了研究。研究表明负荷是重复级现象建立的关键因素之一,在高负荷的情况下,压气机内很快就可到达重复级状态。另外,本文利用重复级流动模型建立了重复级边界条件,在此基础上,利用1.5 级对流场已达到重复级状态的多级流场进行了流场数值模拟,计算结果表明此方法在保证具有较好精度的前提下,可以大量节省计算时间和计算所需内存

关 键 词:轴流式压缩机  边界条件  流场  数值模拟
收稿时间:2/8/1999 12:00:00 AM
修稿时间:1999-02-08

Establishment of Repeating Stage Conditions for Prediction of Axial Compressor Flow Field
Zou Zhengping,Xu Liping and Zhang Zhifang.Establishment of Repeating Stage Conditions for Prediction of Axial Compressor Flow Field[J].Journal of Aerospace Power,2000,15(1):22-26.
Authors:Zou Zhengping  Xu Liping and Zhang Zhifang
Institution:Zou Zhengping 1,Xu Liping 1,Zhang Zhifang 2 2
Abstract:The generation of repeating stage flow pattern in a multistage axial compressor and a simulation model of its flow field are investigated.The results show that the aerodynamic loading is one of the important factors to set up the repeating stage conditions.The flow is quickly reaching the repeating stage conditions as the loading is high.At the same time,a repeating stage boundary conditions are established on the basis of the model.A multi-stage flow field is simulated numerically which is reached the repeating stage conditions,employing 1 5 compressor stages.The results show that this method can improve the convergence as well as save the required memory and time of computation.
Keywords:axial flow compressors  boundary  conditions  flow fields  numerical simulation
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号