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This document discusses the derivation of adjoint equations for a median-dual finite-volume scheme applied to aerodynamic shape optimization, specifically for transonic flows. It highlights the importance of sensitivity analysis in gradient-based optimization, utilizing adjoint methods to efficiently compute gradients of aerodynamic functionals. The authors present a formalism for deriving adjoint equations in the context of the Euler equations and apply it to optimize the RAE 2822 airfoil and ONERA M6 wing

Author

Olivier Amoignon

Language

EN