首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >FLOW AND HEAT TRANSFER MECHANISMS IN A ROTATING COMPRESSOR CAVITY UNDER CENTRIFUGAL BUOYANCY-DRIVEN CONVECTION
【24h】

FLOW AND HEAT TRANSFER MECHANISMS IN A ROTATING COMPRESSOR CAVITY UNDER CENTRIFUGAL BUOYANCY-DRIVEN CONVECTION

机译:离心浮力驱动对流下旋转式压缩机腔中的流动和传热机制

获取原文

摘要

This paper presents a systematic study of flow and heat transfer mechanisms in a compressor disc cavity with an axial throughflow under centrifugal buoyancy-driven convection, comparing with previously published experimental data. Wall-modelled large-eddy simulations are conducted for six operating conditions, covering a range of rotational Reynolds number (3.2 × 10~5 - 2.2 × 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 discs except in the bore flow affected region on the downstream disc cob. The shroud heat transfer Nusselt number-Rayleigh number scaling agrees with that of natural convection under gravity for high Rayleigh numbers. Disc heat transfer is dominated by conduction across unsteady Ekman layers, except on the downstream disc cob. The disc 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.
机译:本文介绍了压缩机盘腔中的流动和传热机制的系统研究,其在离心浮力驱动对流下的轴向流动下,与先前公布的实验数据相比。墙面模型的大涡模拟进行了六种操作条件,覆盖了一系列旋转雷诺数(3.2×10〜5-2.2×10〜6),浮力参数(0.1-0.26)和罗斯比数(0.4 - 0.8) 。考虑了模拟的数值准确性和计算效率。将壁传热预测与具有良好协议水平的测量数据进行比较。恒定的rothalpy核心发生在高埃克特号码中,出现在促进驱动浮力力。腔中的流动是在两个盘上观察到的非稳定层ekman层,除了在下游盘玉米棒上的孔流动影响区域。护罩热转印Nusselt Nultleigh号缩放与高瑞利数的重力下的自然对流相一致。磁盘传热通过在不稳定的EKMAN层中传导,除了下游盘玉米棒外。盘孔传热接近管道流动强制对流相关性。研究了不稳定的流动结构在延伸到轴向流动中的腔体中显示出强的不稳定性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号