喷嘴长宽比和雷诺数对旋流冷却流动与传热特性的影响

杜长河; 范小军; 李亮; 丰镇平

doi:10.7652/xjtuxb201512020

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喷嘴长宽比和雷诺数对旋流冷却流动与传热特性的影响

更新时间：2025-07-09

- 喷嘴长宽比和雷诺数对旋流冷却流动与传热特性的影响
- Effects of Jet Nozzle Aspect Ratio and Reynolds Number on Flow and Heat Transfer Characteristics of Vortex Cooling
- 西安交通大学学报 2015年49卷第12期页码：124-129+143
- 作者机构：
  
  西安交通大学叶轮机械研究所,西安,710049
- 作者简介：
- 基金信息：
- DOI：10.7652/xjtuxb201512020
  中图分类号： TK474.7
- 网络首发：2015-12-10，
  
  纸质出版：2015
- 稿件说明：
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杜长河, 范小军, 李亮, 等. 喷嘴长宽比和雷诺数对旋流冷却流动与传热特性的影响[J]. 西安交通大学学报, 2015,49(12):124-129+143.

Effects of Jet Nozzle Aspect Ratio and Reynolds Number on Flow and Heat Transfer Characteristics of Vortex Cooling[J]. 2015, 49(12): 124-129+143.
杜长河, 范小军, 李亮, 等. 喷嘴长宽比和雷诺数对旋流冷却流动与传热特性的影响[J]. 西安交通大学学报, 2015,49(12):124-129+143. DOI： 10.7652/xjtuxb201512020.

Effects of Jet Nozzle Aspect Ratio and Reynolds Number on Flow and Heat Transfer Characteristics of Vortex Cooling[J]. 2015, 49(12): 124-129+143. DOI： 10.7652/xjtuxb201512020.

摘要

针对叶片前缘冷却流动与传热问题

建立了合理的旋流腔冷却结构。通过求解三维稳态RANS方程和标准k-ω湍流模型

数值分析了喷嘴长宽比和雷诺数对旋流冷却流动和传热的影响。基于数值计算结果对无量纲传热系数Nu、喷嘴长宽比C

和雷诺数Re进行方程拟合

得到旋流冷却的传热关联式。结果表明:冷气从喷嘴进口切向射入旋流腔并形成高速旋流

显著增强换热; 随着喷嘴长宽比从0.2增大到9

旋流外区面积、冷气速度和冷气湍流动能先减小后增大

冷气压力系数先增大后减小; 在大喷嘴长宽比时

Nu沿旋流腔周向和轴向的分布较为均匀; 随着雷诺数的增大

冷气在旋流腔中的流动结构不变

而冷气速度、湍流动能、压力系数和壁面Nu均显著增大; 平均Nu随着雷诺数的增大而显著增大

随着喷嘴长宽比的增大先减小然后增大; 传热关联式与数值计算结果的误差在10%以内

可以准确预测旋流冷却的换热系数。

Abstract

A proper vortex chamber structure is established in terms of blade leading edge cooling. The influence of jet nozzle aspect ratio and Reynolds number on flow field and heat transfer characteristics of vortex cooling is numerically analyzed by means of 3-D steady RANS equations coupled with standard k-ω turbulence model. Based on numerical data

the heat transfer correlations are summarized with respect to the Nusselt number

jet nozzle aspect ratio and Reynolds number. Results show that high speed rotational flow is formed by the impingement air

thus the heat transfer intensity is significantly enhanced. When jet nozzle aspect ratio increases from 0.2 to 9

the outer rotation region

air speed and turbulence kinetic energy decrease at first and then increase

while the static pressure ratio increases at first and then decreases. A larger jet nozzle aspect ratio results in more uniform Nusselt number distribution in the circumferential and axial direction. An increase in Reynolds number leads to pronounced increases in air speed

turbulence kinetic energy

static pressure ratio and wall Nusselt number. However

the flow characteristics are not sensitive to Reynolds number. The globally averaged Nusselt number increases as Reynolds number increases

but decreases at first and then increases as jet nozzle aspect ratio increases. The heat transfer correlation can be used to accurately predict the vortex cooling heat transfer coefficient with a deviation less than 10%.

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references

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LIGRANI P M, HEDLUND C R, THAMBU R, et al. Flow phenomena in swirl chambers [J]. Experiments in Fluids, 1998, 24(3): 254-264.

GLEZER B, MOON H K, O'CONNELL T. A novel technique for the internal blade cooling [C]∥Proceedings of the 1996 ASME Turbo Expo. New York, USA: ASME, 1996: V004T09A015.

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