海军航空工程学院学报2011，Vol.26Issue(4)：361-364,374,5.
无人飞行器外形布局设计及其气动特性计算分析
Configuration Design and Aerodynamic Performance Analysis of an Unmanned Aerial Vehicle
摘要
Abstract
In this paper, a new configuration of an Unmanned Aerial Vehicle （UAV） was designed by conic lofting method and its aerodynamic performances were analyzed. The nodes of UAV geometry was generated and imported to Gambit software to build the grid file which was the foundation of aerodynamic computation. In terms of variant flight conditions, the suitable Computational Fluid Dynamics （CFD） methods were used to calculate the aerodynamic performances of UAV with Fluent software. The longitudinal aerodynamic performances of UAV with the speed of Mach 0.3, 0.6 and 1.3 were computed. The results including lift coefficient, drag coefficient and pitching moment coefficient at different heights were achieved. As a results were analyzed, the calculated data could show the high lift-to-drag ratio and longitudinal stability. In result, the configuration of UAV could satisfy the flying quality with favorable aerodynamic performances.关键词
无人飞行器/气动布局设计/气动特性/计算流体力学Key words
UAV/aerodynamic configuration design/aerodynamic performance/CFD引用本文复制引用
王允良,高永,侯志强..无人飞行器外形布局设计及其气动特性计算分析[J].海军航空工程学院学报,2011,26(4):361-364,374,5.基金项目
国家自然科学基金资助项目 （）
