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

跨音速单转子压气机三维湍流流场的数值计算
引用本文:陈乃兴,黄伟光,周倩.跨音速单转子压气机三维湍流流场的数值计算[J].航空动力学报,1995,10(2):109-112,197.
作者姓名:陈乃兴  黄伟光  周倩
作者单位:中国科学院工程热物理研究所
摘    要:用有限体积表示的三维雷诺平均N-S方程显式格式的时间推进法, 对一个单转子压气机的三维湍流流场进行了计算。方法中应用了Baldwin-Lomax湍流模型。这个单转子压气机是第39届国际燃气轮机会议作为考核三维流场数值方法的盲题。计算结果与实验实测的结果进行了比较, 证明本文提出的方法可以用来验证叶轮机械气动设计。 

关 键 词:三维流动    跨音速压气机    转子    湍流    数值计算
收稿时间:8/1/1994 12:00:00 AM
修稿时间:1994/10/1 0:00:00

NUMERICAL COMPUTATION OF 3D TURBULENT FLOW IN A TRANSONIC SINGLE ROTOR COMPRESSOR
Chen Naixing,Huang Weiguang and Zhou Qian.NUMERICAL COMPUTATION OF 3D TURBULENT FLOW IN A TRANSONIC SINGLE ROTOR COMPRESSOR[J].Journal of Aerospace Power,1995,10(2):109-112,197.
Authors:Chen Naixing  Huang Weiguang and Zhou Qian
Institution:Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100080
Abstract:The 3D turbulent flow in a transonic single rotor is computed numerically by use of an explicit 3D turbulent time-marching Navier-Stokes solver in finite volume form with the option of applying Baldwin-Lomax turbulent model.This rotor served as the blind test case organized by the ASME Turbomachinery Committee.Its purpose was to provide a forum for a careful assessment of the ability of the various turbomachinery CFD codes available to predict the flow field in modern blading.The computational results by the authors' method were compared with the experiment and presented in the present paper.It is demonstrated that the present method can be used for checking the aerodynamical design.
Keywords:Rotors Transonic compressors  Numerical computation  Tree dimensional flow
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