Experimental heat transfer of rib roughened rectangular cooling channels with bleed holes

This thesis examines the advantages of implementing ribs on the mid-chord cooling channels of turbine airfoils. The scaled model of rectangular cross-section channels with aspect ratio of 3 are tested with 5 different configurations. The heat dissipation inside the channel is modelled as a heated wa...

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Online Access:http://hdl.handle.net/2047/D20237820