Stiffened Panel Buckling and Post Buckling Behavior

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F08%3APU79466" target="_blank" >RIV/00216305:26210/08:PU79466 - 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

Stiffened Panel Buckling and Post Buckling Behavior

Original language description

This paper deals with the aluminum stiffened panel load capacity determination and buckling and post buckling behavior description. Sereval methods for the load capacity of the stiffened panel's prediction are used for the designof modern airframe structures. The detailed description of individual methods, the possibility of their utilization and the comparison of the results are the main goal of this research.

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

2008

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

2008

Issue of the periodical within the volume

2

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

5

Pages from-to

50-54

UT code for WoS article

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EID of the result in the Scopus database

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