Effect of Film-Hole Shape on Turbine Blade Heat Transfer Coefficient Distribution
38th, Aerospace sciences meeting ; 2000 ; Reno, NV
2000-01-01
ALL
Paper nos AIAA-2000-0001 to AIAA-2000-1076 with gaps
Conference paper
English
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Effect of Film Injection Location on Local Heat Transfer Coefficient on a Gas Turbine Blade
Online Contents | 1998
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