CFD Simulations Using Reduced Models for Film Cooling Design
2011 (English)In: 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2011, American Institute of Aeronautics and Astronautics, 2011, AiAA 2011-710- p.Conference paper (Other academic)
Film cooling technologies are widely used for attaining high efficiency in gas turbine engines. In this study we have investigated the potential for reduced models to capture different aspects of film cooling by means of CFD at low turn-around time while maintaining the accuracy at a reasonable level. CFD simulations and experiments were carried out for an engine-like setting. Subsequently, the computational domain was reduced in two steps in order to decrease the simulation time. Results for all models are compared with experimental data, including aerodynamic validation, heat transfer coefficient and film effectiveness. The aerodynamic results are very similar for experiments and simulations, and the heat transfer coefficient and film cooling effectiveness showed similarities within the expected range. Thus, this strategy could be very useful for e.g. early vane and film cooling design.
Place, publisher, year, edition, pages
American Institute of Aeronautics and Astronautics, 2011. AiAA 2011-710- p.
Film Cooling, Gas Turbines, CFD
IdentifiersURN: urn:nbn:se:liu:diva-76905DOI: 10.2514/6.2011-710ISBN: 978-1-60086-950-1 (online)OAI: oai:DiVA.org:liu-76905DiVA: diva2:518699
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 4–7 January 2011, Orlando, Florida