COMPUTATIONAL AERODYNAMIC OPTIMIZATION OF LOW-SPEED WING
DOI:
https://doi.org/10.14311/AP.2014.54.0420Abstract
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.Downloads
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Published
2014-12-31
How to Cite
Lahuta, M., Pátek, Z., & Szöllös, A. (2014). COMPUTATIONAL AERODYNAMIC OPTIMIZATION OF LOW-SPEED WING. Acta Polytechnica, 54(6), 420–425. https://doi.org/10.14311/AP.2014.54.0420
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