31th Congress of the International Council of the Aeronautical Sciences

03.4 - Applied Aerodynamics

WING TWIST OPTIMISATION USING AERODYNAMIC SOLVERS OF DIFFERENT FIDELITY

G. Yang¹, A. Da Ronch¹, D. Kharlamov¹, J. Drofelnik¹; ¹University of Southampton, United Kingdom

This paper investigates a benchmark test case of wing twist optimisation using two aerodynamic solvers: SU2 and a hybrid aerodynamic solver, with focus on the effectiveness of optimisation framework and efficiency of these two flow solvers.


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