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Jet Impingement Cooling System on the Pressure Side of Turbine Blade
Applied Mechanics and Materials
This study is to investigate the effectiveness of jet impingement cooling system on the turbine blade pressure side. The objective of this study is to determine the mass blowing rate referred to Reynolds number and the nozzle exit to surface distance which will produce the highest cooling effectiveness which will be shown as Nusselt number. A model of CF6-50 blade is made from mild steel and an experiment to study the jet impingement cooling effectiveness on the pressure side of turbine bladedoi:10.4028/www.scientific.net/amm.695.503 fatcat:2xdhmoln4zdipmh25qjj77hh7m