Szczegóły publikacji
Opis bibliograficzny
Particle swarm based airfoil optimization for sUAV's operating in a low range of Reynold's number / Tom KUSZNIR, Jarosław SMOCZEK // W: MMAR 2017 : 22nd international conference on Methods and Models in Automation and Robotics : 28–31 August 2017, Międzyzdroje, Poland : program, abstracts. — Szczecin : ZAPOL, [2017]. — ISBN: 978-83-7518-844-8. — S. 41. — Pełny tekst na Dysku Flash. — S. 258–262. — Wymagania systemowe: Adobe Reader. — Bibliogr. s. 262, Abstr. — ISBN: 978-1-5386-2402-9. — Toż pod adresem https://ieeexplore-1ieee-1org-1000047po0029.wbg2.bg.agh.edu.pl/stamp/stamp.jsp?tp=&arnumber=8046835
Autorzy (2)
Słowa kluczowe
Dane bibliometryczne
| ID BaDAP | 109123 |
|---|---|
| Data dodania do BaDAP | 2017-10-02 |
| DOI | 10.1109/MMAR.2017.8046835 |
| Rok publikacji | 2017 |
| Typ publikacji | materiały konferencyjne (aut.) |
| Otwarty dostęp |  |
| Konferencja | International Conference on Methods and Models in Automation and Robotics 2017 |
Abstract
The paper focuses on Particle Swarm Optimization of an airfoil model for small unmanned aerial vehicles operating in low Reynolds number. The objective function to be maximized is the lift-to-drag ratio subject to different penalty constraints. The airfoil parameterization is done using Class/Shape function Transformation. Blade Element Momentum Theory is used to develop an optimum hovering propeller with the optimized airfoil and the Clark Y airfoil. The results of the numerical simulation are discussed in the paper. © 2017 IEEE.
