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| 外压式超声速进气道流场的数值模拟 | |
| 引用本文： | 王平,段炼,马洪安.外压式超声速进气道流场的数值模拟[J].飞机设计,2009,29(5):9-12. |
| 作者姓名： | 王平 段炼 马洪安 |
| 作者单位： | 1. 空军航空大学,航空机械工程系,吉林,长春,130022 2. 空军驻京西地区军事代表室,北京,100074 3. 沈阳航空工业学院,动力与能源学院,辽宁,沈阳,110136 |
| 摘 要： | 采用CFD方法对某型外压式超声速进气道流场进行了二维数值计算,叙述了网格生成、边界条件确定方法,控制方程求解收敛技巧以及计算结果的分析.数值计算结果与理论相符较好. |
| 关 键 词： | 超声速进气道 数值模拟 收敛 |
Numerical Simulation of External-Compression Supersonic Inlet Flow Fields |
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| WANG Ping,DUAN Lian,MA Hong-an.Numerical Simulation of External-Compression Supersonic Inlet Flow Fields[J].Aircraft Design,2009,29(5):9-12. | |
| Authors: | WANG Ping DUAN Lian MA Hong-an |
| Institution: | WANG Ping1,DUAN Lian2,MA Hong-an3(1.Aerospace and Mechanical Engineering Department,Aviation University of Air Force,Changchun 130022,China)(2.Air Force Military Delegate Office Located in Western Beijing,Beijing 100074,China)(3.College of Energy and Pow,Shenyang Institute of Aeronautical Engineering,Shenyang 110136,China) |
| Abstract: | In this paper,Method of CFD is used to simulate 2D flow fields for a certain external-compression supersonic inlet.It describes the method of mesh generation,boundary conditions determination,convergence techniques of governing equation,and analyzes simulation result.The numerical results match well with the theoretical. |
| Keywords: | supersonic inlet numerical simulation convergence |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |