Publication detail
The Methodology of Winglet Aerodynamic Design for Ul and VLA Aircraft
POPELA, R. ZIKMUND, P. VANĚK, F. KOUŘIL, M.
Czech title
Metodika aerodynamického návrhu wingletu pro UL a VLA letoun
English title
The Methodology of Winglet Aerodynamic Design for Ul and VLA Aircraft
Type
journal article - other
Language
en
Original abstract
The paper brings methodology description of winglets design for small airplanes. The CFD methods were used to solve aerodynamic wing loading.
Czech abstract
Článek přináší popis metodiky návrhu wingletů pro malé letouny. Metody CFD byly použity k řešení aerodynamického zatížení křídla.
English abstract
The paper brings methodology description of winglets design for small airplanes. The CFD methods were used to solve aerodynamic wing loading.
Keywords in English
winglet design, CFD, load distribution, lift distribution
RIV year
2007
Released
08.11.2007
Location
Praha
ISSN
1211-877X
Journal
Letecký zpravodaj
Volume
2007
Number
3
Pages from–to
52–55
Pages count
3
BIBTEX
@article{BUT43911,
author="Robert {Popela} and Pavel {Zikmund} and František {Vaněk} and Martin {Kouřil},
title="The Methodology of Winglet Aerodynamic Design for Ul and VLA Aircraft",
journal="Letecký zpravodaj ",
year="2007",
volume="2007",
number="3",
month="November",
pages="52--55",
address="Praha",
issn="1211-877X"
}