numerical study of heat transfer in a square channel with and without bleed holes roughened with staggered square ribs
This thesis investigates the internal and external cooling effects on a turbine blade when employing bleed holes between 90° staggered square ribs in the cooling channel of an airfoil. These geometries could have numerous applications in an adjacent channel near the leading edge of the blade to supp...
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| Online Access: | http://hdl.handle.net/2047/D20317970 |