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Acta Polytechnica | Vol.54, Issue.6 | 2017-05-30 | Pages

COMPUTATIONAL AERODYNAMIC OPTIMIZATION OF LOW-SPEED WING

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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COMPUTATIONAL AERODYNAMIC OPTIMIZATION OF LOW-SPEED WING

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Keywords

nonlinear aerodynamics solver computer genetic and evolution optimization algorithm optimization method geometric quantities design of lowspeed wing geometric parameterization of wing

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,.COMPUTATIONAL AERODYNAMIC OPTIMIZATION OF LOW-SPEED WING. 54 (6),.

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