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

PSE方法在后部加载叶栅绕流稳定性分析及转捩预测中的应用
引用本文:董学智,颜培刚,韩万金.PSE方法在后部加载叶栅绕流稳定性分析及转捩预测中的应用[J].航空动力学报,2007,22(9):1492-1498.
作者姓名:董学智  颜培刚  韩万金
作者单位:哈尔滨工业大学,能源科学与工程学院,哈尔滨,150001
摘    要:采用数值求解与实验测量相结合的方法,分析后加载叶栅绕流的稳定性并预测转捩.推导出正交曲线坐标系下三维扰动波的抛物化稳定性方程,在风洞实验中测量叶栅叶片表面的静压分布,并结合测量结果对设计叶栅的流动稳定性进行特征值分析.分析结果表明:(1)后加载叶型能有效推迟转捩,提高叶栅的变冲角特性;(2)当冲角变化时叶顶流动稳定性的变化最显著,负冲角流动稳定,正冲角流动最不稳定.

关 键 词:航空、航天推进系统  边界层流动  稳定性  转捩  后部加载叶型  PSE方法  方法  后部加载  叶栅绕流  流动稳定性  特征值分析  预测  应用  prediction  transition  stability  analysis  boundary  cascade  method  不稳定  变化  特性  冲角  后加载叶型  测量结果  设计
文章编号:1000-8055(2007)09-1492-07
收稿时间:2006/8/24 0:00:00
修稿时间:2006年8月24日

Application of PSE method into aft-load cascade boundary stability analysis and transition prediction
DONG Xue-zhi,YAN Pei-gang and HAN Wan-jin.Application of PSE method into aft-load cascade boundary stability analysis and transition prediction[J].Journal of Aerospace Power,2007,22(9):1492-1498.
Authors:DONG Xue-zhi  YAN Pei-gang and HAN Wan-jin
Institution:School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China;School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China;School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
Abstract:The stability and transition of aft-load blade was analyzed and predicted by combining numerical calculation and experimental measurement.Parabolized stability equation(PSE) of 3D disturbance wave was deducted under orthogonal curvilinear coordinates.The static pressure distribution on blade surface was measured in wind tunnel test,and this result was used for analysis of blade's flow stability.The results show that:(1) aft-load blade can delay efficiently the transition and enhance the variable incidence of blade;(2) the positive incidence is most unsteady and negative incidence is most steady in the event of significant change of flow characteristics of blade tip.
Keywords:aerospace propulsion system  boundary flow  stability  transition  aft-load blade  parabolized stability equation(PSE)method
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