COMPARISON OF TWO-EQUATION TURBULENCE MODELS FOR PREDICTION OF HEAT TRANSFER ON FILM-COOLED TURBINE BLADES
Author:
Publisher
Informa UK Limited
Subject
Condensed Matter Physics,Numerical Analysis
Link
http://www.tandfonline.com/doi/pdf/10.1080/10407789708913895
Reference10 articles.
1. An Experimental Convective Heat Transfer Investigation Around a Film-Cooled Gas Turbine Blade
2. Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades
3. LEADING EDGE FILM-COOLING EFFECTS ON TURBINE BLADE HEAT TRANSFER
4. Discrete-Jet Film Cooling: A Comparison of Computational Results With Experiments
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1. AN ASSESSMENT OF TURBULENCE MODELS FOR PREDICTING CONJUGATE HEAT TRANSFER FOR A TUBINE VANE WITH INTERNAL COOLING CHANNELS;Heat Transfer Research;2015
2. Evaluation of CFD simulations of film cooling performance on a turbine vane including conjugate heat transfer effects;International Journal of Heat and Fluid Flow;2014-12
3. Heat Transfer in Separated Flows on the Pressure Side of Turbine Blades;Numerical Heat Transfer, Part A: Applications;2011-10-15
4. Comparative study of large eddy simulation of film cooling using a dynamic global-coefficient subgrid scale eddy-viscosity model with RANS and Smagorinsky Modeling;International Communications in Heat and Mass Transfer;2011-05
5. Convective heat transfer in cross-corrugated triangular ducts under uniform heat flux boundary conditions;International Journal of Heat and Mass Transfer;2011-01
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