COMPUTATIONAL AERODYNAMIC OPTIMIZATION OF LOW-SPEED WING
Martin Lahuta, Zdeněk Pátek, András Szöllös
Acta Polytechnica · 2014
doi:10.14311/ap.2014.54.0420 (opens in a new tab)
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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.
Abstract licence: CC BY
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