Detail publikace

VUT 001 Marabu Fuselage Design Methodology

MALIŠ, M. URÍK, T. DOUPNÍK, P. ZABLATZKÝ, J.

Anglický název

VUT 001 Marabu Fuselage Design Methodology

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

The article describes the design methodology of an experimental aircraft VUT 001 Marabu. The project is coordinated and partially manufactured by Institute of Aerospace Engineering of Brno University of Technology. The article is focused on design of composite fuselage and describes all phases of realization: initial design, aerodynamic design of aircraft configuration, detailed support structure design, manufacturing technology, and static test. The emphasis is placed on effective modern computer aided design methods used during the project.

Klíčová slova anglicky

composite structure, fuselage design, design methodology

Vydáno

2010-06-10

Nakladatel

Studio Winter Ltd. Prague

Místo

Praha

ISSN

1211-877X

Časopis

Letecký zpravodaj

Ročník

2010

Číslo

2

Strany od–do

2–7

Počet stran

6

BIBTEX


@article{BUT50507,
  author="Michal {Mališ} and Tomáš {Urík} and Petr {Doupník} and Jiří {Zablatzký}",
  title="VUT 001 Marabu Fuselage Design Methodology",
  journal="Letecký zpravodaj",
  year="2010",
  volume="2010",
  number="2",
  pages="2--7",
  issn="1211-877X"
}