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.
1. Boyce, M. P., Gas Turbine Engineering Handbook, Elsevier, Amsterdam, The Netherlands, 2011
2. Koop, W., The Integrated High Performance Turbine Engine Technology (IHPTET) Program, https://ntrs.nasa.gov/citations/19890016803
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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