Flow field numerical simulation method and experimentation validation of air cooling turbine stage

被引：0

作者：

Wei, Gang ^{[1
,2
]}

Wang, Song-Tao ^{[2
]}

Zhou, Shan ^{[1
]}

Zhou, Xun ^{[2
]}

Wang, Zhong-Qi ^{[2
]}

机构：

[1] China Gas Turbine Establishment, Aviation Industry Corporation of China, Chengdu 610500, China

[2] School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China

来源：

Hangkong Dongli Xuebao/Journal of Aerospace Power | 2012年 / 27卷 / 03期

关键词：

Mixing - Trees (mathematics) - Turbine components - Aerodynamics - Computational fluid dynamics - Numerical models - Navier Stokes equations - Gas turbines - Turbomachine blades - Film cooling - Flow fields - Numerical methods;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Using tree order precision Godunoc format with total variation diminishing (TVD) property, free-form surface grid generation technology and divided area grid algorithm, the three-dimensional (3-D) Navier-Stokers (N-S) equations considering cooled air mixing about one type turbine stage were resolved, and the numerical results were comparatively analyzed with the test ones. Through the analysis of the numerical simulation results, the aerodynamic characteristics of the turbine stage were investigated. The results show: the rapid efficient grid generation method considering cooled air mixing and the arbitrary division flow field algorithm can meet the engineering application on the overall performance rapid calculation and flow structure's detailed description of air cooling turbine stage.

引用

页码：651 / 656

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