Publication result detail

The Methodology of Winglet Aerodynamic Design for Ul and VLA Aircraft

POPELA, R.; ZIKMUND, P.; VANĚK, F.; KOUŘIL, M.

Original Title

The Methodology of Winglet Aerodynamic Design for Ul and VLA Aircraft

English Title

The Methodology of Winglet Aerodynamic Design for Ul and VLA Aircraft

Type

Peer-reviewed article not indexed in WoS or Scopus

Original Abstract

The paper brings methodology description of winglets design for small airplanes. The CFD methods were used to solve aerodynamic wing loading.

English abstract

The paper brings methodology description of winglets design for small airplanes. The CFD methods were used to solve aerodynamic wing loading.

Keywords

winglet design, CFD, load distribution, lift distribution

Key words in English

winglet design, CFD, load distribution, lift distribution

Authors

POPELA, R.; ZIKMUND, P.; VANĚK, F.; KOUŘIL, M.

Released

08.11.2007

Location

Praha

ISBN

1211-877X

Periodical

Letecký zpravodaj

Volume

2007

Number

3

State

Czech Republic

Pages from

52

Pages to

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",
  pages="52--55",
  issn="1211-877X"
}