期刊文献+

浅析高空长航时无人机的气动研究问题 被引量:17

A brief discussion of high-altitude long-endurance unmanned aerial vehicle aerodynamic research
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摘要 叙述了高空长航时无人机的现状和作用,讨论了它的主要气动特征,评述了可行的分析、设计技术。认为XFOIL技术具备了处理边界层转捩、分离、分离泡的能力,可望在我国高空长航时无人机的气动设计中发挥一定作用。 In this paper are presented the function and development situation of high-altitude long-endurance unmanned aerial vehicle,discussed the main aerodynamic characteristics,commented the feasible analysis and design technique.It is thought that the XFOIL code has the ability to deal with the boundary layer transition,flow separation and the separation bubble,and expected it will play an important role in aerodynamic design of our high-altitude long-endurance unmanned aerial vehicle.
出处 《流体力学实验与测量》 CSCD 北大核心 2004年第3期1-5,共5页 Experiments and Measurements in Fluid Mechanics
关键词 无人机 气动特征 边界层转捩 分离模拟 XFOIL软件 unmanned aerial vehicle aerodynamic characteristics boundary layer transition separation simulation XFOIL code
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参考文献4

  • 1CEBECI T,BESNARD E,CHEN H H.Calculation ofmulti-element airfoil flows,including flap well[R] .AIAA-96-0056.
  • 2RICHARD E. A computer program for the design and analysis of low-speed airfoils [J]. NASA TM 80210.
  • 3DRELA M, GILES M B.Viscous-inviscid analysis of transonic and low reynolds number airfoils [J].AIAA J-vol-25-pp 1347-1355,1987-10.
  • 4URPO J, RAMESH K A.A fast and robust viscous/inviscid interaction code for wing flowfield calculations [R].AIAA-99-3139.

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