检索结果-南通市图书馆

Analysis of swirling flow effects on the characteristics of unsteady hot-streak migration

Chinese Journal of Aeronautics 2016年第6期29卷 1469-1476页

作者： Wang Jingyu Ge Ning Sheng Chunhua Nanjing University of Aeronautics and Astronautics Nanjing 210016China Sun Yat-Sen University Guangzhou 510275China The University of Toledo OH 43606USA

The temperature of flow at the combustor exit is inherently non-uniform and the hot fluid is called hot-streak. An in-house CFD software, NUAA-Turbo, was used to carry out 3D unsteady simulations on the PW-Esingle-stage high-pressure turbine. The hot-streak effect based on real stator and combustor counts was approximately evaluated by the contraction/dilatation method on the interface. The unsteady attenuation and migration process of hot-streaks in the turbine passage were well captured. The general performance parameters for different circumferential positions of hot-streaks were relatively consistent. Then, the influences of hot-streaks on blade surface temperature were investigated by comparing results under hot-streak and uniform inflow conditions. Unsteady simulations with combined inlet hot-streak and swirling flow show that the core of a hot-streak migrates to the tip under the influence of a positive swirl, while the phenomenon is just opposite with a negative swirl. Therefore, the heat transfer environment of rotor blades shows great differences with different directions of inlet swirl.

关键词： High pressure turbine hot-streak Interface contraction/dilatation Swirling flow Unsteady flow

来源：

维普期刊数据库

同方期刊数据库评论

在线全文

学校读者我要写书评

暂无评论

The influence of inlet swirl intensity and hot-streak on aerodynamics and thermal characteristics of a high pressure turbine vane

引用

Chinese Journal of Aeronautics 2021年第11期34卷 66-78页

作者： Zakaria MANSOURI Riyadh BELAMADI ABYLSEN Science&Technology Rhone Alpes Grenoble 38000France Ecole Superieure de Technologies Industrielles(ESTI) Annaba 23000Algeria

In modern gas turbines,the High Pressure Turbine(HPT)is exposed to an extreme thermal environment due to the burned gases leaving the *** burned gases are characterized by flow and temperature distortions that effect the aerodynamics and heat transfer of the *** purpose of this paper is to investigate numerically the effect of the intensity of the swirling flow combined with the temperature non-uniformity‘‘hot-streak"(H-S)on the aerothermal performances of a HPT Nozzle Guide Vane(NGV).The investigations are conducted on the solid untwisted NGV annular cascade developed in NASA Lewis Research *** swirl intensities(|S_(n)|=0,0.1,0.25 and 0.5),two swirl orientations(positive and negative)and two hot-streaks(rounded and radial)at the NGV inlet are *** simulations are done by solving the Reynolds Averaged Navier-Stokes(RANS)equations using ANSYS-CFX *** results show that the H-S with swirl undergoes twisting following the orientation of the *** H-S twist is aggressive under positive swirl compared to the negative swirl *** inlet swirl generates a new secondary flow structure,so called Swirl Vortex(SV),which induces more aerodynamic *** aerodynamic efficiency under negative swirl found to be higher than that under positive *** maximum temperature on the vane surface is controlled by the radial transport of the SV towards the endwalls.

关键词： Aerodynamics Heat transfer hot-streak HP turbine NGV Swirl intensity

来源：

维普期刊数据库

同方期刊数据库评论

在线全文

学校读者我要写书评

暂无评论

欢迎您,

建议与咨询留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

时间限定

文献类型

馆藏选择

核心期刊

语言

文献类型

帮助

文字说明：

检索规则说明：

检索范例：

分类表

所选分类

限定检索结果

文献类型

馆藏范围

日期分布

学科分类号

主题

机构

作者

语言

在线全文

在线全文

请选择保存的检索档案：

请选择收藏分类：

通借通还

欢迎您,

建议与咨询 留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

时间限定

文献类型

馆藏选择

核心期刊

语言

文献类型

帮助

文字说明：

检索规则说明：

检索范例：

分类表

所选分类

限定检索结果

文献类型

馆藏范围

日期分布

学科分类号

主题

机构

作者

语言

在线全文

在线全文

请选择保存的检索档案： 新增检索档案 确定 取消

请选择收藏分类： 新增自定义分类 确定 取消

通借通还

建议与咨询留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

请选择保存的检索档案：

请选择收藏分类：