Numerical study of Louver cooling scheme on gas turbine airfoils
This work presents the performance of a louver film-cooling scheme under different operating conditions. The louver cooling scheme consists of a bend by which the coolant going through the flow passage is redirected from vertical to horizontal direction before being injected into the mainstream thro...
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| Format: | Others |
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2008
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| Online Access: | http://spectrum.library.concordia.ca/975197/1/NR45686.pdf Zhang, Xuezhi <http://spectrum.library.concordia.ca/view/creators/Zhang=3AXuezhi=3A=3A.html> (2008) Numerical study of Louver cooling scheme on gas turbine airfoils. PhD thesis, Concordia University. |