The application of similarity theory for heat transfer investigation in rotational internal cooling channel

被引:11
|
作者
Xu, Guoqiang [1 ,2 ]
Li, Yang [1 ,2 ]
Deng, Hongwu [1 ,2 ]
Li, Haiwang [1 ,2 ]
Yu, Xiao [3 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Natl Key Lab Sci & Technol Aeroengine Aerothermod, Beijing 100191, Peoples R China
[2] Beijing Univ Aeronaut & Astronaut, Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China
[3] Aviation Ind Corp China, Shenyang Aeroengine Design & Res Inst, Shenyang 110015, Peoples R China
关键词
Similarity theory; Heat transfer; Rotating channel; Dissimilar radius; Scaled-up channel; 2-PASS SQUARE CHANNEL; SERPENTINE PASSAGES; SMOOTH; PREDICTION; MODEL;
D O I
10.1016/j.ijheatmasstransfer.2015.01.108
中图分类号
O414.1 [热力学];
学科分类号
摘要
Full-scale test for turbine blade internal cooling is difficult for laboratory researches. The original turbine blade channel is always proportionally scaled up to laboratory-scale channel, as well as its hydraulic diameter and rotating radius. But the proportion scale of radius is too large for any rotating rig to operate the test, and thus the insufficient rotating radius causes incomplete similarity application. Because of the dissimilar radius induced incomplete similarity, heat transfer results obtained in laboratory-scale channel cannot be directly used by actual turbine blade design process. Therefore, this paper deals with this problem and numerically studies the influence of incomplete similarity through a rotating square channel with smooth walls and radially outward flow. Dimensionless parameters analysis demonstrates that the radius ratio (RID) only shows influence on the buoyancy number (Buo) which causes much smaller buoyancy number for dissimilar model. Thus, three models with various scales and rotating radius are built. Model 1 is the original channel simplified from actual turbine blade internal cooling channel; Model 2 (similar model) and Model 3 (experimental model) are the corresponding scaled-up channels from Model 1 with complete similar radius and insufficient radius respectively. And two correction methods (variable radius and variable wall temperature) are developed to revise the influence caused by incomplete similarity of Model 3. Variable radius is used to vary rotating radius and variable wall temperature is used to vary wall temperature. The simulation is completed using commercial CFD solver and k-omega turbulent model. Result shows that the conventional application of similarity theory can predict heat transfer well for complete similar model (Model 2), but with a large deviation for dissimilar model (Mode 3). Given the same Re and Ro, the smaller Buo in Model 3 causes over 17% deviation heat transfer result. Then, the two revised methods concerning the effect of rotational radius ratio and wall temperature ratio are detailedly discussed, and both of them show less than 3% deviation in heat transfer distribution results. The detailed revised steps are also provided for both methods. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:98 / 109
页数:12
相关论文
共 50 条
  • [31] COOLING OPTIMISATION THEORY, PART 2: OPTIMUM INTERNAL HEAT TRANSFER COEFFICIENT DISTRIBUTION
    Kirollos, Benjamin
    Povey, Thomas
    ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 5A, 2015,
  • [32] Heat transfer in a cooling channel with vortex generators
    Chyu, MK
    Ding, H
    JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 1997, 119 (02): : 206 - 206
  • [33] INVESTIGATION ON HEAT TRANSFER CHARACTERISTICS OF A COOLING CHANNEL WITH DENSE ARRAY OF ANGLED RIB TURBULATORS
    Hagari, Tomoko
    Ishida, Katsuhiko
    Takeishi, Ken-ichiro
    Oda, Yutaka
    Kitada, Hiroki
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 4, PTS A AND B, 2012, : 387 - +
  • [34] An Experimental Investigation of Heat Transfer Characteristics for Steam Cooling in a Rectangular Channel with Parallel Ribs
    MA Chao
    CHEN Xiaoling
    WANG Jianfei
    ZANG Shusheng
    JI Yongbin
    JournalofThermalScience, 2014, 23 (05) : 454 - 464
  • [35] Numerical investigation on flow and heat transfer mechanism of corrugated cooling channel in turbine blades
    Wu, Chenhan
    Yang, Xiaoquan
    Tang, Xiaolong
    Ding, Jue
    Weng, Peifen
    PHYSICS OF FLUIDS, 2023, 35 (02)
  • [36] An Experimental Investigation of Heat Transfer Characteristics for Steam Cooling in a Rectangular Channel with Parallel Ribs
    Ma Chao
    Chen Xiaoling
    Wang Jianfei
    Zang Shusheng
    Ji Yongbin
    JOURNAL OF THERMAL SCIENCE, 2014, 23 (05) : 454 - 464
  • [37] An experimental investigation of heat transfer characteristics for steam cooling in a rectangular channel with parallel ribs
    Chao Ma
    Xiaoling Chen
    Jianfei Wang
    Shusheng Zang
    Yongbin Ji
    Journal of Thermal Science, 2014, 23 : 454 - 464
  • [38] Similarity theory and dimensionless numbers in heat transfer
    Marin, E.
    Calderon, A.
    Delgado-Vasallo, O.
    EUROPEAN JOURNAL OF PHYSICS, 2009, 30 (03) : 439 - 445
  • [39] LTCC substrates with internal cooling channel and heat exchanger
    Zampino, MA
    Adluru, H
    Liu, YQ
    Jones, WK
    2003 INTERNATIONAL SYMPOSIUM ON MICROELECTRONICS, 2003, 5288 : 505 - 510
  • [40] Heat transfer enhancement by inserting a radiation enhancement plate in turbine blade internal cooling channel
    Liu, Jie
    Wang, Jiabing
    Yang, Kun
    INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2023, 143