Volume 32 Issue 1
Jan.  2017
Turn off MathJax
Article Contents
Experiment on pressure distribution and flow resistance characteristics of internal lamilloy.[J]. Journal of Aerospace Power, 2017, 32(1): 14-21. doi: 10.13224/j.cnki.jasp.2017.01.003
Citation: Experiment on pressure distribution and flow resistance characteristics of internal lamilloy.[J]. Journal of Aerospace Power, 2017, 32(1): 14-21. doi: 10.13224/j.cnki.jasp.2017.01.003

Experiment on pressure distribution and flow resistance characteristics of internal lamilloy.

doi: 10.13224/j.cnki.jasp.2017.01.003
  • Received Date: 2015-05-19
  • Publish Date: 2017-01-28
  • Two kinds of lamilloy models with different percentages of film hole opening were experimentally studied at the Reynolds numbers of 1×104-6×104,target surface, impingement surface and pressure coefficients of pinfins surface,local and total loss coefficients of impingement jet, arounding flow,effusion were experimented to explore the mechanism of flow loss. Results showed that,the pressure distributions were characterized by the second maximum value because of the transition from an accelerating stagnation region flow to a decelerating wall jet. The low pressure coefficients on the target and impingement surfaces were caused by the sink of two jets and the backflow, respectively. The pressure coefficients distributions on two rows of pinfins relatively far away from the impingement hole were significantly affected by Reynolds numbers. At the Reynolds number less than or equal to 3×104, the pressure distributions were similar with flow across cylinder. At the Reynolds number greater than or equal to 4×104, it also had characteristics of backflow. The effusion loss coefficients were biggest, the impingement jet loss coefficients were smallest and the arounding flow loss coefficients were moderate. As the percentages of opening decreased one half, the effusion loss coefficients of film holes increased at least 4 times while the loss coefficients of impingement jet loss and arounding flow had slight changes.

     

  • loading
  • [1]
    Vershure R W,Jr.Engine demonstration testing of cooled laminated axial turbine[R].AIAA 791229,1979.
    [2]
    Wear J D,Trout A M.Design and preliminary results of a semitranspiration cooled (lamilloy) liner for a highpressure combustor[R].Las Vegas:AIAA/SAE 14th Joint Propulsion Conference,1978.
    [3]
    Nealy D A,Reider S B.Evaluation of laminated porous wall materials for combustor liner cooling[J].Journal for Engineering for Power,1978,102(2):268-276.
    [4]
    梁春华,王鸣,刘殿春.战斗机发动机涡轮叶片层板发散冷却技术的发展[J].航空制造技术,2013(9):90-93. LIANG Chunhua,WANG Ming,LIU Dianchun.Development of laminated transpirationcooled turbine blade for flight engine[J].Aeronautical Manufacturing Technology,2013(9):90-93.(in Chinese)
    [5]
    孔满昭,朱惠人,原和朋.应用瞬态液晶测量技术研究层板内部换热特性[J].航空动力学报,2009,24(2):340-346. KONG Manzhao,ZHU Huiren,YUAN Hepeng.Research on heat transfer characteristics of lamilloy internal surfaces using transient liquid crystal technique[J].Journal of Aerospace Power,2009,24(2):340-346.(in Chinese)
    [6]
    胡娅萍,卢元丽,吉洪湖,等.层板冷却涡轮叶片前缘内部流动与传热特性实验研究[J].航空动力学报,2014,29(2):240-249. HU Yaping,LU Yuanli,JI Honghu,et al.Experimental on flow and heat transfer characteristics inside leading edge of lamilloy[J].Journal of Aerospace Power,2014,29(2):240-249.(in Chinese)
    [7]
    李江海.层板冷却特性的研究[D].西安:西北工业大学,2005. LI Jianghai.Investigation of cooling characteristics of lamilloy[D].Xi'an:Northwestern Polytechnical University,2005.(in Chinese)
    [8]
    全栋梁,刘松龄,李江海.层板冷却结构强化换热机理[J].航空动力学报,2004,19(6):860-865. QUAN Dongliang,LIU Songling,LI Jianghai.Numerical investigation on mechanism of heat transfer augmentation in lamilloy [J].Journal of Aerospace Power,2004,19(6):860-865.(in Chinese)
    [9]
    全栋梁.层板叶片冷却特性研究[D].西安:西北工业大学,2005. QUAN Dongliang.Investigation of cooling characteristics of lamilloy turbine blade[D].Xi'an:Northwestern Polytechnical University,2005.(in Chinese)
    [10]
    郁新华,全栋梁,刘松龄.层板结构内部流场数值模拟研究[J].航空学报,2004,25(6):534-539. YU Xinhua,QUAN Dongliang,LIU Songling.Numerical simulation of the internal flow in lamilloy[J].Acta Aeronautical Astronautica Sinica,2004,25(6):534-539.(in Chinese)
    [11]
    袁星,吕东.扰流柱几何参数对层板流阻和换热特性的影响[J].航空动力学报,2009,24(5):1016-1021. YUAN Xing,L Dong.Effects of pinfins geometry parameters on flow resistance and heat transfer characteristics of lamilloy[J].Journal of Aerospace Power,2009,24(5):1016-1021.(in Chinese)
    [12]
    陶智,吕东,丁水汀,等.扰流柱直径对倾斜出气孔层板内流动与换热影响的数值研究[J].航空动力学报,2007,22(4):540-546. TAO Zhi,L Dong,DING Shuiting,et al.Numerical study on the influences of pinfin diameter on the flow resistance and heat transfer of leaning vent hole lamilloy[J].Journal of Aerospace Power,2007,22(4):540-546.(in Chinese)
    [13]
    李谦,王建华,吴向宇,等.冷却介质在层板内流动特性研究[J].实验流体力学,2007,21(4):18-21. LI Qian,WANG Jianhua,WU Xiangyu,et al.An investigation of coolant flow performance within laminated plate[J].Journal of Experiments in Fluid Mechanics,2007,21(4):18-21.(in Chinese)
    [14]
    李冰.层板冷却结构内部流场显示与换热特性研究[D].西安:西北工业大学,2007. LI Bing.Investigation of flow visualization and heat transfer characteristics of lamilloy[D].Xian:Northwestern Polytechnical University,2007.(in Chinese)
    [15]
    赵乃芬,谭晓茗,李业芳,等.高致密多孔层板结构选型研究[J].推进技术,2014,35(11):1517-1522. ZHAO Naifen,TAN Xiaoming,LI Yefang,et al.Research on structures of highdensity laminate porous plate[J].Journal of Propulsion Technology,2014,35(11):1517-1522.(in Chinese)
    [16]
    全栋梁,郁新华,刘松龄,等.层板冷却结构流阻特性的实验与数值模拟[J].推进技术,2003,24(5):425-428. QUAN Dongliang YU Xinhua,LIU Songling,et al.Experimental and numerical investigation of internalflow resitance characteristics in laminate porous plates[J].Journal of Propulsion Technology,2003,24(5):425428.(in Chinese)
    [17]
    郁新华,董志锐,刘松龄,等.层板模型流阻特性的研究[J].推进技术,2000,21(4):47-50. YU Xinhua,DONG Zhirui,LIU Songling.Study for flowresistance characteristics of the modelled laminated porous wall[J].Journal of Propulsion Technology,2000,21(4):47-50.(in Chinese)
    [18]
    陶智,魏豪杰,丁水汀,等.典型层板冷却结构中流体流阻与换热特性的实验研究[J].航空动力学报,2007,22(2):194-198. TAO Zhi,WEI Haojie,DING Shuiting,et al.Experimental investigation of flow resistance and heat transfer characteristics of typical lamilloy models[J].Journal of Aerospace Power,2007,22(2):194-198.(in Chinese)
    [19]
    全栋梁,刘松龄,李江海,等.多孔层板冷却有效性的研究[J].航空动力学报,2004,19(4):520-524. QUAN Dongliang,LIU Songling,LI Jianghai,et al.Experimental investigation of cooling effectiveness of laminate porous plates[J].Journal of Aerospace Power,2004,19(4):520-524.(in Chinese)
    [20]
    李冰,朱惠人,于芳芳.层板结构叶片温度场的工程计算[J].机械设计与制造,2008(11):19-21. LI Bing,ZHU Huiren,YU Fangfang.Calculation of wall temperature of lamilloy blade[J].Machinery Design and Manufacture,2008(11):19-21.(in Chinese)
    [21]
    Cho H H,Rhee D H.Local heat/mass transfer measurement on the effusion plate in impingment/effusion cooling systems[J].Journal of Turbomachinery,2001,123(3):601-608.
    [22]
    Bernard A,Brizzi L E,Bousgarbies J L.Study of several jets impinging on a plate wall:visualizations and laser velocimetry investigations[J].Journal of Fluids Engineering,1999,121(4):808-812.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1004) PDF downloads(466) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return