翼/短舱/吊架气动特性及其动力影响数值研究

李强; 汪明生

翼/短舱/吊架气动特性及其动力影响数值研究

李强^,,
汪明生

南京航空航天大学能源与动力学院,南京 210016

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- 文章访问数: 1981
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- 被引次数: 0
出版历程
- 收稿日期: 2011-08-25
- 刊出日期: 2012-07-28

Numerical simulation of wing/nacelle/pylon aerodynamic characteristics and their changes under powered condition

LI Qiang^,,
WANG Ming-sheng

College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016 China

摘要

摘要: 应用计算流体动力学(CFD)数值模拟方法对DLR-F6模型分别在通流及动力条件下翼/短舱/吊架(W-N-P)组合体部分的气动干扰特性进行研究.结果表明:组合体相互干扰引起的干扰通道附增激波及短舱后部逆压导致的涡流增加了短舱外罩阻力,降低了机翼升力;动力条件较通流条件,F6短舱外罩阻力降低,机翼升阻力特性在零度攻角时有所提高.
- 短舱 /
- 气动干扰 /
- 动力条件 /
- 流动分析 /
- 涡流
Abstract: Based on DLR-F6 model,the wing -nacelle-pylon (W-N-P)configuration dynamic characteristics were calculated by computational fluid dynamics(CFD) method under through flow condition and powered condition respectively.The results show that the interference configuration passage shock wave and nacelle vortex would increase nacelle overall drag and reduce wing lift.The resistance would be lower under power condition compare with that under through flow condition.
- nacelle /
- mutual interference /
- powered condition /
- flow simulation /
- vortex

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参考文献(12)

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