Volume 31 Issue 11
Nov.  2016
Turn off MathJax
Article Contents
YANG Ke, WEN Jie, XU Guo-qiang. Numerical investigation of flow and heat transfer characteristics in rotating square U-duct[J]. Journal of Aerospace Power, 2016, 31(11): 2567-2574. doi: 10.13224/j.cnki.jasp.2016.11.002
Citation: YANG Ke, WEN Jie, XU Guo-qiang. Numerical investigation of flow and heat transfer characteristics in rotating square U-duct[J]. Journal of Aerospace Power, 2016, 31(11): 2567-2574. doi: 10.13224/j.cnki.jasp.2016.11.002

Numerical investigation of flow and heat transfer characteristics in rotating square U-duct

doi: 10.13224/j.cnki.jasp.2016.11.002
  • Received Date: 2015-03-11
  • Publish Date: 2016-11-28
  • k-ω SST (shear stress transport) two-equation turbulence model was used to analyze the flow and heat transfer characteristics in rotating square U-duct at different inlet Reynolds numbers (10000~60000) and rotation numbers (0~2.013). Results show that both in stationary and rotating state, Nusselt numbers are augmented with the increase of inlet Reynolds number. Comparing with stationary state, at the same Reynolds number, the intensity of heat transfer in radial outward passage is dramatically enhanced by rotating, while the radial inward passage is just enhanced a little. Rotation number influences the U-duct heat transfer through changing the values of Coriolis force and buoyancy force. Coriolis force enhances greatly the heat transfer of trailing surface in radial outward passage, while the leading surface weakens. Buoyancy force causes flow separation in the vicinity of the wall, so it alters the heat transfer characteristics. In different positions of the radial inward passage, the heat transfer intensity of the leading surface firstly decreases and then increases with the rise of rotation number. The critical rotation numbers got by calculation are in good agreement with the experimental results. The product of dimensionless distance parameter and critical rotation is a constant.

     

  • loading
  • [1]
    曹玉璋.航空发动机传热学[M].北京:北京航空航天大学出版社,2005.
    [2]
    Akella K V,Han J C.Impingement cooling in rotating two-pass rectangular passages[J].Journal of Thermophysics and Heat Transfer,1998,12(4):582-588.
    [3]
    Bons J P,Kerrebrock J L.Complementary velocity and heat transfer measurement in a rotating cooling passage with smooth walls[R].ASME Paper 98-GT-464,1998.
    [4]
    Han J C,Dutta S,Ekkad S.Gas turbine heat transfer and cooling technology[M].Boca Raton:CRC Press,2000.
    [5]
    Han J C.Turbine blade cooling studies at texas A&M university[J].Journal of Thermophysics and Heat Transfer,2006,20(2):161-187.
    [6]
    Han J C,Huh M.Recent studies in turbine blade internal cooling[J].Journal of Heat Transfer Research,2010,41(8):803-828.
    [7]
    Qiu L,Deng H W,Sun J N,et al.Pressure drop and heat transfer in rotating smooth square U-duct under high rotation numbers[J].International Journal of Heat and Mass Transfer,2013,66:543-552.
    [8]
    Deng H W,Qiu L,Sun J N,et al.Heat transfer study in rotating smooth square U-duct at high rotation numbers[J].International Journal of Heat and Mass Transfer,2013,66:733-741.
    [9]
    Banhoof B,Tomm U,Johnson B V,et al.Heat transfer predictions for rotating U-shaped coolant passages with skewed ribs and with smooth walls[R].ASME Paper 97-GT-162,1997.
    [10]
    Lin Y L,Shih T I,Chyu M K,et al.A numerical study of flow and heat transfer in a smooth and ribbed U-duct with and without rotation[J].Journal of Heat Transfer,2001,123(10):219-232.
    [11]
    Stephens M A,Shih T I,Civinskas K C.Computations of flow and heat transfer in a rotating U-shaped square duct with smooth walls[R].AIAA 96-3161,1996.
    [12]
    Stephens M A,Shih T I.Computations of compressible flow and heat transfer in a rotating duct with inclined ribs and a 180 degree bend[R].ASME Paper 97-GT-192,1997.
    [13]
    Shih T I,Lin Y L,Stephens M A.Flow and heat transfer in a ribbed U-Duct under typical engine conditions[R].ASME Paper 98-GT-213,1998.
    [14]
    Iacovides H,Launder B E.Parametric and numerical study of fully developed flow and heat transfer in rotating rectangular ducts[J].Journal of Turbomachinery,1991,113(3):331-338.
    [15]
    Medwell J O,Morris W D,Xia J Y,et al.Aninvestigation of convective heat transfer in a rotating coolant channel[J].Journal of Turbomachinery,1991,113(3):354-359.
    [16]
    Chen H C,Jang Y J,Han J C.Computation of flow and heat transfer in rotating two-pass square channels by a Reynolds stress model[R].ASME Paper 99-GT-174,1999.
    [17]
    Huster A I,Biringen S.Direct numerical simulation of turbulent flow in a square duct[J].Journal of Fluid Mechanics,1993,257:65-95.
    [18]
    Gavrilakis S.Numerical simulation of low Reynolds number turbulent flow through a straight square duct[J].Journal of Fluid Mechanics,1992,244:101-129.
    [19]
    Madabhushi R K,Vanka S P.Large eddy simulation of turbulence-driven secondary flow in a square duct[J].Physics of Fluids:A,1991,3(11):2734-2745.
    [20]
    Murata A,Mochizuki S.Effect of cross-sectional aspect ratio on turbulent heat transfer in an orthogonally rotating rectangular smooth duct[J].International Journal of Heat and Mass Transfer,1999,42(20):3803-3814.
    [21]
    Pallares J,Davidosn L.Large eddy simulation of turbulent flow in a rotating square duct[J].Physics of Fluids,2000,12(11):2878-2894.
    [22]
    Li Y,Deng H W,Xu G Q,et al.Effect of passage orientation on heat transfer in rotating smooth square U-duct at high rotation numbers[R].ASME Paper GT2014-25188,2014.
    [23]
    Dutta S,Andrews M J,Han J C.Prediction of turbulent heat transfer in rotating smooth square ducts[J].International Journal of Heat and Mass Transfer,1996,39(12):2505-2514.
  • 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 (1117) PDF downloads(656) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return