Film cooling effectiveness on the suction side of a turbine blade in a two dimensional laminar flow /
The study of film cooling effectiveness on the suction side of a CF6-50 model turbine using numerical method. The study is limited to two dimensional laminar flow with asumption og incompressible flow, adiabatic condition and govern by steady-state form of governing equation. The result of film cool...
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Sekudai : UTM,
1994
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