Steady-state experiment and numerical simulation on flow and heat transfer of a rotating cavity with axial flow

被引:0
作者
Zhang Z. [1 ]
Luo X. [1 ,2 ]
Cao N. [1 ]
机构
[1] National Key Laboratory of Science and Technology on Aero-Engine and Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University, Beijing
[2] Collaborative Innovation Center for Advanced Aeroengine, Beihang University, Beijing
来源
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics | 2021年 / 47卷 / 11期
基金
中国国家自然科学基金;
关键词
Axial flow; Cone disk; Flow structure; Heat transfer characteristics; Rotating cavity;
D O I
10.13700/j.bh.1001-5965.2020.0426
中图分类号
学科分类号
摘要
The steady-state experiment and numerical simulation were carried out to investigate the flow structure and heat transfer characteristics in the rotating cavity with axial flow. By changing the axial flow coefficient, rotating Reynolds number, etc., the radial distribution of temperature and Nusselt number on both sides of the disk and the inner side of the disk cone under different working conditions was explored. The results show that: the radial distribution of temperature on both sides of the disk is concave, and the heat transfer intensity on the upwind side of the disk is generally higher than that on the leeward side. The cone disk conducts heat conduction to the disks on both ends, and the radial distribution of the wall surface temperature is high in the middle and low on both sides. With the increase of the axial flow coefficient, the gas convection inside the disk cavity was intensified, the radial arm and vortex pair became explicit, and the heat transfer effect on the surface of the rotating disk and the cone disk was enhanced. The flow heat transfer characteristics in the cavity of the rotating disk are influenced by forced convection and Rayleigh-Benard like convection. © 2021, Editorial Board of JBUAA. All right reserved.
引用
收藏
页码:2369 / 2377
页数:8
相关论文
共 17 条
[1]  
OWEN J M, PINCOMBE J R., Vortex breakdown in a rotating cylindrical cavity, Journal of Fluid Mechanics, 90, 1, pp. 109-127, (1979)
[2]  
FARTHING P R, LONG G A, OWEN J M, Et al., Rotating cavity with axial throughflow of cooling air: Flow structure, Journal of Turbomachinery, 114, 1, pp. 237-246, (1992)
[3]  
ALEXIOU A., Flow and heat transfer in gas turbine h. p. compressor internal air systems, (2000)
[4]  
BOHN D E, DEUTSCH G N, SIMON B, Et al., Flow visualisation in a rotating cavity with axial throughflow, ASME Turbo Expo: Power for Land, Sea, & Air, (2000)
[5]  
TIAN S Q, TAO Z, DING S T, Et al., Investigation of flow instability in rotating cavity with axial throughflow of cooling air, Journal of Beijing University of Aeronautics and Astronautics, 31, 4, pp. 393-396, (2005)
[6]  
TIAN S Q, TAO Z, DING S T, Et al., Numerical investigation on heat transfer in a rotating cavity with axial throughflow of cooling air, Journal of Aerospace Power, 20, 4, pp. 656-661, (2005)
[7]  
TIAN S Q, TAO Z, DING S T, Et al., Investigation of Rayleigh-Benard-like convection stabilities in rotating cavity with axial throughflow of cooling air, Journal of Thermal Science and Technology, 2, 3, pp. 260-265, (2003)
[8]  
PITZ D B, CHEW J W, MARXEN O., Effect of an axial throughflow on buoyancy-induced flow in a rotating cavity, International Journal of Heat and Fluid Flow, 80, (2019)
[9]  
FARTHING P R, LONG C A, OWEN J M, Et al., Rotating cavity with axial throughflow of cooling air: Heat transfer, Journal of Turbomachinery, 114, 1, pp. 229-236, (1992)
[10]  
OWEN J M, POWELL J., Buoyancy induced flow in a heated rotating cavity, Journal of Engineering for Gas Turbines and Power, 128, 1, pp. 128-134, (2006)