Film Cooling from a Row of Holes Supplemented with Anti Vortex Holes
Film cooling is a technique employed to protect the external surface of gas turbine blades from the hot mainstream gas by ejecting the internal coolant air through discrete holes or slots at several locations on the blade exterior surface. Passing the coolant through conventional cylindrical holes c...
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| Format: | Others |
| Language: | en |
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LSU
2007
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| Online Access: | http://etd.lsu.edu/docs/available/etd-07122007-232839/ |