Flow and Heat Transfer Mechanisms in a Rotating Compressor Cavity Under Centrifugal Buoyancy-Driven Convection

被引:20
|
作者
Gao, Feng [1 ,3 ]
Chew, John W. [2 ]
机构
[1] Beihang Univ, Fluid & Acoust Engn Lab, Aeroengine Res Inst, Beijing 102206, Peoples R China
[2] Univ Surrey, Fac Engn & Phys Sci, Guildford GU2 7XH, Surrey, England
[3] Univ Surrey, Guildford, Surrey, England
基金
英国工程与自然科学研究理事会;
关键词
AXIAL THROUGHFLOW; COOLING AIR;
D O I
10.1115/1.4052649
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper presents a systematic study of flow and heat transfer mechanisms in a compressor disk cavity with an axial throughflow under centrifugal buoyancy-driven convection, comparing with previously published experimental data. Wall-modeled large-eddy simulations (WMLES) are conducted for six operating conditions, covering a range of rotational Reynolds number (3.2 x 10(5) - 2.2 x 10(6)), buoyancy parameter (0.11-0.26), and Rossby number (0.4-0.8). Numerical accuracy and computational efficiency of the simulations are considered. Wall heat transfer predictions are compared with measured data with a good level of agreement. A constant rothalpy core occurs at high Eckert number, appearing to reduce the driving buoyancy force. The flow in the cavity is turbulent with unsteady laminar Ekman layers observed on both disks except in the bore flow affected region on the downstream disk cob. The shroud heat transfer Nusselt number-Rayleigh number scaling agrees with that of natural convection under gravity for high Rayleigh numbers. Disk heat transfer is dominated by conduction across unsteady Ekman layers, except on the downstream disk cob. The disk bore heat transfer is close to a pipe flow forced convection correlation. The unsteady flow structure is investigated showing strong unsteadiness in the cavity that extends into the axial throughflow.
引用
收藏
页数:11
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