Numerical and experimental investigationg of a turbine guide vane with conjugate heat transfer method

Author:

Liu Youhong1,Luo Yifu1,Ding Yulin1,Guo Jia1,Xiao Changgeng1

Affiliation:

1. National Key Laboratory of Science and Technology on Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University, Beijing, China

Abstract

Three-dimensional steady-state conjugate heat transfer numerical method was utilized to study the flow and heat transfer characteristics of a turbine guide vane. In experiment, a real-sized turbine vane model and corresponding test section were designed. We verified the simulation accuracy of different turbulence models, coupling with transition model and limiter factor in conjugate heat transfer method. Compared with the experimental results, the results indicated that the SST model shows better accuracy and economy than other models studied in this paper.

Publisher

National Library of Serbia

Subject

Renewable Energy, Sustainability and the Environment

Reference24 articles.

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3. Hennecke, D., Turbine Blade Cooling in Aeroengines, Von Karman Institute Lecture Series, Sint-Genesins-Rode, Belgium, 1982

4. Nealy, D., et al., Measurements of Heat Transfer Distribution over the Surfaces of Highly Loaded Turbine Nozzle Guide Vanes, Journal of Engineering Gas Turbines Power, 106 (1984), 1, pp. 149-158

5. Arts, T., et al., Aerothermal Performance Measurements and Analysis of a Two-Dimensional High Turning Rotor Blade, Journal of Turbomachinery, 120 (1998), 3, pp. 494-499

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