Experimental and Computational Investigation of Flow Structure in Buoyancy-Dominated Rotating Cavities

被引:11
作者
Fazeli, Seyed Mostafa [1 ]
Kanjirakkad, Vasudevan [1 ]
Long, Christopher [1 ]
机构
[1] Univ Sussex, Sch Engn & Informat, Thermofluid Mech Res Ctr, Falmer BN1 9QT, England
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2021年 / 143卷 / 07期
关键词
AXIAL THROUGHFLOW; COOLING AIR;
D O I
10.1115/1.4049482
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The flow and heat transfers inside high-pressure (HP) compressor rotating cavities are buoyancy driven and are known to be extremely difficult to predict. The experimental data of laser-Doppler anemometry (LDA) measurements inside an engine representative cavity rig are presented in this paper. Traverses using a two component LDA system have been carried out in the shaft bore and the cavity regions in order to map the axial and tangential velocity components. The velocity data are collected for a range of Rossby, Rotational, and Axial Reynolds numbers, Ro, Re-theta, and Re-z,0:08 < Ro < 0.64, 7 x 10(5) < Re-theta < 2.83 x 10(6), and 1.2 x 10(4) < Re-z < 4.8 x 10(4), respectively, and for values of the buoyancy parameter beta Delta T, 0:284 < beta Delta T < 0:55. Numerical study using unsteady Reynolds-averaged-Navier-Stokes (URANS) simulations has been carried out to elucidate flow details for a few selected cases. The experimental results revealed that the Swirl number (X-k) varies from a value< 1 near the bore to near solid body rotation at increased radii within the cavity. The analysis of frequency spectrum of the tangential velocity inside the cavities has also shown the existence of pairs of rotating and contrarotating vortices. There is generally satisfactory agreement between measurements and computational fluid dynamics (CFD) simulations. There is also convincing evidence of two or more separate regions in the flow dominated by the bore flow and rotation.
引用
收藏
页数:10
相关论文
共 22 条
  • [1] Heat transfer in high-pressure compressor gas turbine internal air systems: A rotating disc-cone cavity with axial throughflow
    Alexiou, A
    Hills, NJ
    Long, CA
    Turner, AB
    [J]. EXPERIMENTAL HEAT TRANSFER, 2000, 13 (04) : 299 - 328
  • [2] Alexiou A., 2000, PhD Thesis
  • [3] Atkins NR, 2014, ASME TURBO EXPO TURB, V5C
  • [4] Bohnhoff D. R., 2000, 2000 ASAE Annual International Meeting, Milwaukee, Wisconsin, USA, 9-12 July 2000, P1
  • [5] Dweik Z., 2009, GT200959969 ASME, DOI [10.1115/GT2009-59969, DOI 10.1115/GT2009-59969]
  • [6] Dweik Z., 2009, GT200959978 ASME, DOI [10.1115/GT2009-59978, DOI 10.1115/GT2009-59978]
  • [7] ROTATING CAVITY WITH AXIAL THROUGHFLOW OF COOLING AIR - FLOW STRUCTURE
    FARTHING, PR
    LONG, CA
    OWEN, JM
    PINCOMBE, JR
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1992, 114 (01): : 237 - 246
  • [8] ROTATING CAVITY WITH AXIAL THROUGHFLOW OF COOLING AIR - HEAT-TRANSFER
    FARTHING, PR
    LONG, CA
    OWEN, JM
    PINCOMBE, JR
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1992, 114 (01): : 229 - 236
  • [9] King M.P., 2005, GT200568948 ASME, DOI [10.1115/GT2005-68948, DOI 10.1115/GT2005-68948]
  • [10] Flow measurements inside a heated multiple rotating cavity with axial throughflow
    Long, C. A.
    Miche, N. D. D.
    Childs, P. R. N.
    [J]. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2007, 28 (06) : 1391 - 1404