COMPUTATIONAL AERODYNAMIC OPTIMIZATION OF LOW-SPEED WING

Martin Lahuta, Zdeněk Pátek, András Szöllös

Abstract


An optimization method consisting of genetic and evolution optimization algorithm and a solver using nonlinear aerodynamics was applied on design of low-speed wing. Geometric parameterization of wing uses standard geometric quantities commonly used for the description of wing geomtery. The method seems to provide good teliable results at low computer capacity requirements.

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ISSN 1210-2709 (Print)
ISSN 1805-2363 (Online)
Published by the Czech Technical University in Prague