Multi-Fidelity Aerodynamic Optimization of an Airfoil at a Transitional Low Reynolds Number
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8th Symposium on Applied Aerodynamics and Design of Aerospace Vehicles, Royal Orchid Resort and Convention BangaloreCite As
Priyanka,R., Sivapragasam,M. and Narahari,H. K. (2018) Multi-Fidelity Aerodynamic Optimization of an Airfoil at a Transitional Low Reynolds Number, 8th Symposium on Applied Aerodynamics and Design of Aerospace Vehicles, Royal Orchid Resort and Convention Bangalore.