Vortex Dissipation Due to Airfoil-Vortex Interaction

Efficient Design Exploration for Civil Aircraft Using a Kriging-Based Genetic Algorithm

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14/01/20 "Engineering Optimization in Aircraft Design" Aerodynamic Design at Univ. of Tokyo

MULTI-POINT DESIGN OF A SUPERSONIC WING USING MODIFIED PARSEC AIRFOIL REPRESENTATION

Aerodynamic design of Aircraft”