Numerical Simulation for Aerodynamic Characteristics of Low Altitude and Subsonic Flight Vehicle

摘要：

In order to analyze the drag characteristics of the vehicle having different war head and empennage, the computational fluid dynamics numerical simulation was used. The method was based on fully hexahedral mesh and threedimensional Navier-Stokes equations and Spalart-Allmaras turbulence model. Through numerical simulation the flow field structures and computational aerodynamic characteristics were obtained. The results showed that using Kaman figure war head and proper trapeziform empennage can reduce the drag characteristics of the missile and the results will provide evidence to optimize the configuration of the missile in engineering design.

关键词： drag characteristics:numerical simulation stabilization:wrap around empennage:trapeziform empennage

作者: Yanli MA Yi JIANG Jiguang HAO Bowei LIU

作者单位: Department of Aerospace Engineering,Beijing Institute of Technology,Beijing,China

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 555-558

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）