Evaluation of CFD simulations of film cooling performance on a turbine vane including conjugate heat transfer effects
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference28 articles.
1. Albert, J.E., Bogard, D.G., 2011. Measurements of adiabatic film and overall cooling effectiveness on a turbine vane pressure side with a trench. In: Proceedings of ASME Turbo Expo, GT2011-46703, Vancouver, Canada.
2. Dees, J.E., Bogard, D.G., Ledezma, G.A., Laskowski, G.M., Tolpadi, A.K., 2010. Experimental measurements and computational predictions for an internally cooled simulated turbine vane with 90 degree rib turbulators. In: Proceedings of ASME Turbo Expo, Glasgow, GT2010-23004, UK.
3. Dees, J.E., Bogard, D.G., Ledezma, G.A., Laskowski, G.M., Tolpadi, A.K., 2010. Momentum and thermal boundary layer development on an internally cooled turbine vane. In: Proceedings of ASME Turbo Expo 2010, Glasgow, GT2010-23008, UK.
4. Dees, J.E., Bogard, David G., Ledezma, Gustavo A., Laskowski, Gregory M., 2011. The effects of conjugate heat transfer on the thermal field above a film cooled wall. In: Proceedings of ASME Turbo Expo, GT2011-46617, Vancouver, Canada.
5. Dobrowolski, L.D., Bogard, D.G., Piggush, J., Kohli, A., 2009. Numerical simulation of a simulated film cooled turbine blade leading edge including conjugate heat transfer effects. In: ASME International Mechanical Engineering Congress & Exposition, IMECE2009-11670, Lake Buena Vista, USA, 2009.
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