Abstract

This paper has the objective to analyze passive flow control technologies that can reduce the shock wave intensity and thus the interference drag in the strut-wing junction, in transonic flight. Two possible flow control devices were investigated by means of CFD, Kuchemann Carrot [...]

Abstract

The paper investigates a robust optimisation for detail design of active shock control bump on a transonic Natural Laminar Flow (NLF) aerofoil using a Multi-Objective Evolutionary Algorithm [...]