Heat Transfer and Flow Characteristics in Rib-/Deflector-Roughened Cooling Channels with Various Configuration Parameters

被引:15
|
作者
Xie, Gongnan [1 ]
Zheng, Shaofei [1 ]
Sunden, Bengt [2 ,3 ]
机构
[1] Northwestern Polytech Univ, Xian 710072, Shaanxi, Peoples R China
[2] Lund Univ, Div Heat Transfer, Dept Energy Sci, Lund, Sweden
[3] Northwestern Polytech Univ, Xian 710072, Shaanxi, Peoples R China
基金
中国国家自然科学基金;
关键词
PRESSURE-DROP CHARACTERISTICS; TRANSFER ENHANCEMENT; RECTANGULAR CHANNELS; SQUARE; PERFORMANCE; DUCTS; ORIENTATION; ARRAY;
D O I
10.1080/10407782.2014.916122
中图分类号
O414.1 [热力学];
学科分类号
摘要
The present paper deals with a detailed numerical investigation of the turbulent flow inside a stationary rib-/deflector-roughened cooling channel. Various downstream-shaped deflectors including sloping-board deflectors [Cases A1, A2], guide-shaped deflectors [Cases B1, B2], and drop-shaped deflectors [Cases C1, C2] and configuration parameters such as channel aspect ratio (AR=0.5, 1 and 2), and rib-pitch-to-rib-height ratio (P/e=5, 8, and 10) are investigated. The main objective is to design an appropriate deflector to improve the flow characteristics in the wake of the deflectors and guide the flow between two neighboring rib turbulators to enhance the heat transfer performance. A quasi-three-dimensional flow structure, supported by the stream tracer field in some planes, is established to improve and deepen the understanding as well as the analysis of the complex flow field in the rib-/deflector-roughened channels. In addition, the thermal performance corresponding to various rib-pitch-to-rib-height ratios and aspect ratios emphasizes the role of the configuration parameters in the heat transfer and flow resistance performance. The results demonstrate that the deflectors trip the boundary layer and blend the fluid flow, and that the sloping board deflectors contribute to enlarging the turbulence level of the whole cooling channel, more than in the wake region. It is found that Cases A1 and A2 provide the best heat transfer performance, while Case C1 presents the largest thermal enhancement factor Nu/Nu(0)/(f/f(0))(1/3) at high Reynolds number. The wide-aspect-ratio channel with deflectors and large pitch-to-height ratio ribs exhibits much better heat transfer performance.
引用
收藏
页码:140 / 169
页数:30
相关论文
共 50 条
  • [31] Film Cooling Extraction Effects on the Aero-Thermal Characteristics of Rib Roughened Cooling Channel Flow
    Cukurel, Beni
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2018, 140 (08):
  • [32] FILM COOLING EXTRACTION EFFECTS ON THE AERO-THERMAL CHARACTERISTICS OF RIB ROUGHENED COOLING CHANNEL FLOW
    Cukurel, B.
    Selcan, C.
    Arts, T.
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 4, PTS A AND B, 2012, : 229 - 241
  • [33] Film Cooling Extraction Effects on the Aero-Thermal Characteristics of Rib Roughened Cooling Channel Flow
    Cukurel, Beni
    Selcan, Claudio
    Arts, Tony
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2013, 135 (02):
  • [34] Effect of rib orientation on heat transfer and flow characteristics of mist/steam in square channels
    Gong, Jianying
    Ma, Chenxi
    Lu, Jiaqi
    Gao, Tieyu
    INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2020, 118 (118)
  • [35] HEAT TRANSFER CHARACTERIZATION INSIDE A ROTATING RIB ROUGHENED COOLING CHANNEL WITH MULTIPLE HEATED WALLS
    Lorenzon, Andrea
    Cucit, Elica
    Casarsa, Luca
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 7A, 2020,
  • [36] Conjugate heat transfer analysis of a rotor blade with rib-roughened internal cooling passages
    Takahashi, Toshihiko
    Watanabe, Kazunori
    Sakai, Takayuki
    Proceedings of the ASME Turbo Expo 2005, Vol 3 Pts A and B, 2005, : 275 - 284
  • [37] Effect of main and secondary flows on heat transfer in a rib-roughened internal cooling channel
    Çakan, M
    Arts, T
    FOURTH INTERNATIONAL SYMPOSIUM ON EXPERIMENTAL AND COMPUTATIONAL AEROTHERMODYNAMICS OF INTERNAL FLOWS, VOL I, PROCEEDINGS, 1999, : 141 - 150
  • [38] Effects of rib arrangements on heat transfer and flow behavior in a rectangular rib-roughened passage: Application to cooling of gas turbine blade trailing edge
    Kiml, R
    Mochizuki, S
    Murata, A
    JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2001, 123 (04): : 675 - 681
  • [39] 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):
  • [40] Local heat transfer in rotating square-rib-roughened and smooth channels with jet impingement
    Hsieh, SS
    Tsai, HH
    Chan, SC
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2004, 47 (12-13) : 2769 - 2784