24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-2.7.5

AERODYNAMIC DESIGN OPTIMIZATION USING UNSTRUCTURED NAVIER-STOKES EQUATIONS ADJOINT METHOD

H- J. Kim, K. Nakahashi
Tohoku University, Sendai 980-8579, Japan

Keywords: aerodynamic design, adjoint method, high lift device

For efficient aerodynamic design optimizations, an adjoint code is developed from an unstructured Navier-Stokes solver.

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