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Prediction of Film Cooling Effectiveness on a Gas Turbine Blade Leading Edge Using ANN and CFD
Prediction of Film Cooling Effectiveness on a Gas Turbine Blade Leading Edge Using ANN and CFD
2018
J. O. Dávalos
J.C. García
G. Urquiza
A. Huicochea
O. de Santiago
Keywords:
Aerospace engineering
Leading edge
Turbine blade
Engineering
Automotive engineering
Computational fluid dynamics
Design of experiments
gas turbines
Correction
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