COMPUTATIONAL AERODYNAMIC OPTIMIZATION OF LOW-SPEED WING

Authors

  • Martin Lahuta
  • Zdeněk Pátek Výzkumný a zkušební letecký ústav, a.s.
  • András Szöllös Výzkumný a zkušební letecký ústav, a,s, Beranových 130, 199 05 Praha – Letňany, Czech Republic

DOI:

https://doi.org/10.14311/AP.2014.54.0420

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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Author Biography

Zdeněk Pátek, Výzkumný a zkušební letecký ústav, a.s.

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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

Issue

Vol. 54 No. 6 (2014)

Section

Articles