翼/短舱/吊架气动特性及其动力影响数值研究
Numerical simulation of wing/nacelle/pylon aerodynamic characteristics and their changes under powered condition
-
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.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.
-
Key words:
- nacelle /
- mutual interference /
- powered condition /
- flow simulation /
- vortex
-
[1] Rumsey C L,Rivers S M,Morrison J H.Study of CFD variation on transport configurations from the second drag-prediction workshop .AIAA 2004-394,2004. [2] Oliveira G L,Trapp L G,Puppin-Macedo A.Integration methodology for regional jet aircraft with underwing engines .AIAA 2003-934,2003. [3] Peng S H,Eliasson P.A comparison of turbulence models in prediciton of flow around the DLR-F6 aircraft configuration .AIAA 2004-4718,2004. [4] LI Jie,CHEN Fengwei,LI Qin,et al.CFD application to airframe/propulsion integration for civil aircraft .AIAA 2000-2228,2000. [5] De Souza A M,Da Silveira Neto A.Parametric analysis of different nacelle positions in the DLR-F6 modal by means of the CFD++ code .AIAA 2008-7053,2008. [6] 陈科甲,白俊强,朱军.发动机短舱对翼身组合体跨音速气动特性影响研究[J].航空计算技术 2010,40(1):63-66. CHEN Kejia,BAI Junqiang,ZHU Jun.Research on transonic aerodynamic performance impact of the engine nacelle[J].Aeronautical Computing Technique 2010,40(1):63-66.(in Chinese) [7] Chen H C,Yu N J,Rubert P E.Flow simulations for general nacelle configurations using Euler equations .AIAA 83-0539,1983. [8] Hirose N,Asai K,Lkawa K,et al.3-D Euler flow analysis of fanjet engine and turbine powered simulator with experimental comparison in transonic speed .AIAA 89-1835,1989. [9] LI Jie,LI Qin,CHEN Fengwei,et al.3-D flow simulations for general powered engine nacelles using Euler equations .AIAA 98-0929,1998. [10] 张美红,王志栋.CFD技术在带动力飞机气动设计中的应用[J].民用飞机设计与研究,2004,(4):52-55. ZHANG Meihong,WANG Zhidong.The useage of CFD method on plane design under power condition[J].Civil Aircarft Design and Research,2004(4):52-55.(in Chinese) [11] 谭兆光,陈迎春,李杰等.机体/动力装置一体化分析中的动力影响效应数值模拟[J].航空动力学报,2009,24(8):1766-1772. TAN Zhaoguang,CHEN Yingchun,LI Jie,et al.Numerical simulation method for powered effects in airframe/propulsion integration analysis[J].Journal of Aerospace Power,2009,24(8):1766-1772.(in Chinese) [12] Brodersen D,Stürmer A.Drag prediction of engine-airframe interference effects using unstructured Navier-Stokes calculations .AIAA 2001-2414,2001.
点击查看大图
计量
- 文章访问数: 1830
- HTML浏览量: 4
- PDF量: 699
- 被引次数: 0