Initial Segment of Terminal Homing Projectiles Aerodynamic Simulation Based on Fluent

摘要：

Make use of Fluent of CFD software, we carry though computation of aerodynamics of the initial segment of a terminal homing projectile in different Mach number and different attack angle and gained movement trend of lift coefficient、drag coefficient and pitching moment coefficient with variety of Mach number and attack angle. The results indicate the computation result could offer basis and data reference for more accurately production of firing table of terminal homing projectile.

关键词： FLUNT terminally-guided projectile aerodynamic simulation

作者: Wang Liwei Pang Yingliang Tian Hao

作者单位: Department of Aeronautic Electronic Engineering, The First Aeronautic Institute of Air Force, Xinyan Department of Artillery Engineering,Ordnance Engineering College,Shijiazhuang, 050003,China

会议类型: 国际会议

会议名称: 第八届国际测试技术研讨会(8th International Symposium on Test and Measurement)

会议地点: 重庆

会议语种:英文

页码: 973-976

在线出版日期: 2009-08-01（万方平台首次上网日期，不代表论文的发表时间）