Detail publikačního výsledku

The Aerodynamics Loads of the Wing-Winglet Configuration for UL and VLA Aircraft

VANĚK, F.; KOUŘIL, M.

Originální název

The Aerodynamics Loads of the Wing-Winglet Configuration for UL and VLA Aircraft

Anglický název

The Aerodynamics Loads of the Wing-Winglet Configuration for UL and VLA Aircraft

Druh

Článek recenzovaný mimo WoS a Scopus

Originální abstrakt

The determination of so-called "air loads" is one of the first and basic tasks of the solving team in the process of designing aircraft. The paper describes the use of the CFD analysis results in the determination of various aerodynamic loads cases of the wing-winglet configuration for UL and VLA aircraft.

Anglický abstrakt

The determination of so-called "air loads" is one of the first and basic tasks of the solving team in the process of designing aircraft. The paper describes the use of the CFD analysis results in the determination of various aerodynamic loads cases of the wing-winglet configuration for UL and VLA aircraft.

Klíčová slova

aerodynamics, winglet, CFD, load distribution, lift distribution

Klíčová slova v angličtině

aerodynamics, winglet, CFD, load distribution, lift distribution

Autoři

VANĚK, F.; KOUŘIL, M.

Rok RIV

2010

Vydáno

31.10.2008

Nakladatel

VZLU

Místo

Praha

ISSN

1211-877X

Periodikum

Letecký zpravodaj

Svazek

2008

Číslo

2

Stát

Česká republika

Strany od

30

Strany do

34

Strany počet

4

BibTex

@article{BUT47664,
  author="František {Vaněk} and Martin {Kouřil}",
  title="The Aerodynamics Loads of the Wing-Winglet Configuration for UL and VLA Aircraft",
  journal="Letecký zpravodaj",
  year="2008",
  volume="2008",
  number="2",
  pages="30--34",
  issn="1211-877X"
}