HEAT TRANSFER IN A ROTATING RIB-ROUGHENED WEDGE-SHAPED U-DUCT

被引:0
|
作者
Ding, Liang [1 ]
Tian, Shuqing [1 ]
Deng, Hongwu [2 ]
机构
[1] AECC Commercial Aircraft Engine Co LTD, Shanghai Ctr Res Commercial Aircraft Engine Engn, Shanghai 200241, Peoples R China
[2] Beijing Univ Aeronaut & Astronaut, Sch Energy & Power Engn, Natl Key Lab Sci & Technol Aeroengine Aerothermod, Beijing 100191, Peoples R China
关键词
2-PASS SQUARE DUCT; FLOW DEVELOPMENT; FLUID-FLOW; PRESSURE MEASUREMENTS; STRONG CURVATURE; CHANNELS; LDA; 45-DEGREES; FRICTION; BEND;
D O I
暂无
中图分类号
O414.1 [热力学];
学科分类号
摘要
Heat transfer in a rotating two-pass trapezium-shaped channel, with staggered 90-deg ribs on both leading and trailing surfaces is experimentally investigated. The hydraulic diameter of the first and second pass is 24.5 mm and 16.9 mm, respectively. The inlet Reynolds number and rotational speed range from 10000 to 50000 and zero to 1000 rpm, respectively, which results in the inlet rotation number varying from zero to 1.0. The heated copper plate technique is employed to measure the regional averaged heater transfer coefficients. Pressure drops are measured by newly designed rotating pressure measurements module. Both ribbed cases and smooth cases are compared to present rib enhancement effect. For non-rotating result, the results show that the trailing surface presents much higher heat transfer than other cases due to the special wedge-shaped geometry. The ribbed wedge-shaped achieves enhanced regional heat transfer performances than the smooth case at all locations. Compared with the non rotating results in the first pass, heat transfer on both trailing and leading surfaces is enhanced except for the position near the turn region, but weakened on outer surface in stream-wise direction. And at high rotation numbers, the highest maximum heat transfer on railing surface happens at a location of approximately X/D=10. In the first pass, rotation always enhances heat transfer on the trailing surface as rotation number increases and the rotation-to-stationary Nusselt number ratio reaches to 2.0 at the rotation number of 0.5. The leading and outer surfaces both have a critical rotation number located at Ro(c)=0.05.
引用
收藏
页数:12
相关论文
共 50 条
  • [21] Heat (mass) transfer in a diagonally oriented rotating two-pass channel with rib-roughened walls
    Park, CW
    Yoon, C
    Lau, SC
    JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2000, 122 (01): : 208 - 211
  • [22] Shape optimization of rib-roughened surface to enhance turbulent heat transfer
    Kim, KY
    Kim, SS
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2002, 45 (13) : 2719 - 2727
  • [23] Effect of Entrance Geometry on Heat Transfer in a Rib-Roughened Rectangular Channel
    Satta, Francesca
    Tanda, Giovanni
    Venturino, Giulio
    HEAT TRANSFER ENGINEERING, 2022, 43 (07) : 623 - 637
  • [25] Experimental study of flow and heat transfer in rib-roughened rectangular channels
    Olsson, CO
    Sunden, B
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 1998, 16 (04) : 349 - 365
  • [26] Heat transfer in a rotating smooth wedge-shaped channel with lateral fluid extraction
    Tao, Zhi
    Qiu, Lu
    Deng, Hongwu
    APPLIED THERMAL ENGINEERING, 2015, 87 : 47 - 55
  • [27] Heat transfer and pressure drop measurements in rib-roughened rectangular ducts
    Gao, XF
    Sundén, B
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2001, 24 (1-2) : 25 - 34
  • [28] Heat transfer study in rotating smooth square U-duct at high rotation numbers
    Deng, Hongwu
    Qiu, Lu
    Tao, Zhi
    Tian, Shuqing
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2013, 66 : 733 - 744
  • [29] LES ANALYSIS OF FLOW AND HEAT TRANSFER IN A RIB-ROUGHENED DUCT IN CLOCKWISE AND ANTI-CLOCKWISE ROTATION REGIMES
    Salvagni, Alessandro
    Borello, Domenico
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2017, VOL 5A, 2017,
  • [30] Flow Structure and Heat Transfer of Jet Impingement on a Rib-Roughened Flat Plate
    Alenezi, Abdulrahman H.
    Almutairi, Abdulrahman
    Alhajeri, Hamad M.
    Addali, Abdulmajid
    Gamil, Abdelaziz A. A.
    ENERGIES, 2018, 11 (06):