Analytical and Experimental Approaches to Airfoil-Aircraft Design Integration

Kailash C. Misra استاد مشاور , Ndaona Chokani استاد مشاور , Ashok Gopalarathnam استاد راهنما

aircraft performance , low speed flow , newton method , drag polar , optimization , drag bucket , Aircraft , Wind tunnel , Laminar flow , XFOIL , cruise flap , low-drag range , automatic flap , design integration , trailing-edge flap , aeronautical , general aviation , pressure distributions , UAV , trim considerations , stagnation point , surface pressure sensing , Design , NLF , airfoil , low reynolds number , Camber , aerospace engineering , thin airfoil theory , trim effects , Subsonic , airfoil model construction