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基于粒子轨迹的结冰风洞收缩段优化设计数值模拟

丛成华 彭强 汪伏波 符澄

丛成华, 彭强, 汪伏波, 符澄. 基于粒子轨迹的结冰风洞收缩段优化设计数值模拟[J]. 航空动力学报, 2012, 27(7): 1555-1561.
引用本文: 丛成华, 彭强, 汪伏波, 符澄. 基于粒子轨迹的结冰风洞收缩段优化设计数值模拟[J]. 航空动力学报, 2012, 27(7): 1555-1561.
CONG Cheng-hua, PENG Qiang, WANG Fu-bo, FU Cheng. Numerical sumulation on optimization design of contraction section in icing wind tunnel based on droplet trajectory[J]. Journal of Aerospace Power, 2012, 27(7): 1555-1561.
Citation: CONG Cheng-hua, PENG Qiang, WANG Fu-bo, FU Cheng. Numerical sumulation on optimization design of contraction section in icing wind tunnel based on droplet trajectory[J]. Journal of Aerospace Power, 2012, 27(7): 1555-1561.

基于粒子轨迹的结冰风洞收缩段优化设计数值模拟

基金项目: 空气动力学国家重点实验室基金(JBKY09040205)

Numerical sumulation on optimization design of contraction section in icing wind tunnel based on droplet trajectory

  • 摘要: 为了研究收缩段型面和液滴轨迹特性对结冰风洞流场品质与结冰试验效果的重要影响,获得收缩段的优化设计参数,采用数值模拟方法,使用二维简化模型对3m×2m结冰风洞收缩段的流场特性进行了研究,对几种典型收缩曲线的流场进行了计算,对比了收缩曲线对沿轴向压力分布、出口截面速度分布、不同粒径云雾粒子的极限释放距离及试验段入口云雾粒子分布的影响,结果表明:三次曲线与xm为0.4的五次曲线不能满足流场合格指标,其他曲线流场特性差别不大,维氏曲线具有最小极限释放距离,在收缩段出口,三次曲线和五次曲线粒子包络面积最大,综合比较,xm为0.5的五次曲线能有效兼顾流场均匀性、极限释放距离和收缩段出口粒子包络面积比.

     

  • [1] Reehorst A L,Ibrahim M.Investigation of water droplet trajectories within the NASA icing research tunnel .NASA-TM-107023,1995.
    [2] Hancir P,Anderson A,Loth E.Computations of droplet distributions in the NASA icing research tunnel .AIAA-2000-0101,2000.
    [3] 刘政崇,廖达雄.高低速风洞气动与结构设计[M].北京:国防工业出版社,2003.
    [4] Tsien H S.On the design of the contraction cone for a wind tunnel[J].Journal of the Aeronautical Sciences.1943,10(2):68-70.
    [5] Bossel H H.Computation of axisymmetric contractions[J].AIAA Journal,1969,7(10):2017-2020.
    [6] Chmielewski G E.Boundary layer considerations in the design of aerodynamic contractions[J].Journal of Aircraft,1974,11(8):435-438.
    [7] Mikhail M N.Optimum design of wind tunnel contractions[J].AIAA Journal,1979,17(5):471-477.
    [8] Batill S M.Aerodynamic design of high contraction ratio,subsonic wind tunnel inlets .AIAA-84-0416,1984.
    [9] Bell J,Mehta R.Contraction design for small low speed wind tunnels .NASA-CR-177488,1989.
    [10] SU Yaoxi.Flow analysis and design of three-dimensional wind tunnel contractions[J].AIAA Journal,1991,29(11):1912-1920.
    [11] Wolf T.Design of a variable contraction for a full-scale automotive wind tunnel[J].Journal of Wind Engineering and Industrial Aerodynamics,1995,56(1):1-21.
    [12] 刘卫红.轴对称收缩段设计研究[J].空气动力学学报 1998,16(2):250-254. LIU Weihong.The design and study of the axisymmetric convergent section[J].Acta Aerodynamica Sinica,1998,16(2):250-254.(in Chinese)
    [13] Fang F M,Chen J C,Hong Y T.Experimental and analytical evaluation of flow in a square-to-square wind tunnel contraction[J].Journal of Wind Engineering and Industrial Aerodynamics,2001,89(3/4):247-262.
    [14] 李国文.风洞收缩段曲线气动性能研究[J].实验流体力学,2009,23(4):73-77. LI Guowen.Study of the performance of contractive curve for the wind tunnel[J].Journal of Experiments in Fluid Mechanics,2009,23(4):73-77.(in Chinese)
    [15] 李素循.一个设计收缩管道的方法[J].力学学报,1979(4):367-373. LI Suxun.A method on the design of contraction ducts[J].Chinese Journal of Theoretical and Applied Mechanics,1979(4):367-373.(in Chinese)
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出版历程
  • 收稿日期:  2011-08-24
  • 刊出日期:  2012-07-28

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