Numerical Analysis of Axisymmetric Nozzle Aerodynamic Characteristics

摘要：

　　Method of CFD is used to simulate flow fields for a certain Axisymmetric nozzle,The paper describes the grid adaption,boundary conditions determination as well as RNG k-ε model application,and analyzes the nozzle aerodynamic characteristics.The numerical results match well with test data.

关键词： numerical analysis nozzle aerodynamic characteristics

作者: WANG Ping LIU Xue-shan WANG Yuan-da WANG Xiao-kun

作者单位: Aeronautical Mechanical Engineering Department, Aviation University of Air Force, 2222 Nanhu Road, Changchun, 130022, P.R.China

会议类型: 国际会议

会议名称: the 2012 International Conference on Frontiers of Mechanical Engineering and Materials Engineering (机械工程与材料工程国际会议())

会议地点: 香港

会议语种:英文

页码: 324-327

在线出版日期: 2012-07-27（万方平台首次上网日期，不代表论文的发表时间）