OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F06%3APU71207" target="_blank" >RIV/00216305:26210/06:PU71207 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

čeština

Original language name

OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING

Original language description

In modern aircraft structural design, the high accuracy calculation to obtain the highest efficiency of the structure is possible through the use of computer analysis. A system of computer programs to optimize and analyze skin-stringer panel for fuselageand lifting surfaces (wing and empennage structures) is being developed at the Institute of aerospace engineering, FME, BUT now. This paper deals with the optimum design of the reinforced panel which means Skin - stringer Panel. This form of construction is a logical development of the necessity of providing a continuous surface for an airplane, combined with the requirement that the weight of structure should be as small as possible.

Czech name

OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING

Czech description

In modern aircraft structural design, the high accuracy calculation to obtain the highest efficiency of the structure is possible through the use of computer analysis. A system of computer programs to optimize and analyze skin-stringer panel for fuselageand lifting surfaces (wing and empennage structures) is being developed at the Institute of aerospace engineering, FME, BUT now. This paper deals with the optimum design of the reinforced panel which means Skin - stringer Panel. This form of construction is a logical development of the necessity of providing a continuous surface for an airplane, combined with the requirement that the weight of structure should be as small as possible.

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

2006

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

2006

Issue of the periodical within the volume

3

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

4

Pages from-to

42-45

UT code for WoS article

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EID of the result in the Scopus database

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