VUT 001 Marabu Fuselage Design Methodology

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F10%3APU89275" target="_blank" >RIV/00216305:26210/10:PU89275 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

VUT 001 Marabu Fuselage Design Methodology

Original language description

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 aideddesign methods used during the project.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

<a href="/en/project/1M0501" target="_blank" >1M0501: Aerospace Research Centre</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

2010

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

2010

Issue of the periodical within the volume

2

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

6

Pages from-to

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UT code for WoS article

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EID of the result in the Scopus database

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