COMPARISON OF THREE TYPES OF IMPERFECTIONS APPLIED DURING BUCKLING ANALYSIS OF CYLINDRICAL SHELL UNDER COMPRESSIVE LOAD
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F13%3APU104401" target="_blank" >RIV/00216305:26210/13:PU104401 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
COMPARISON OF THREE TYPES OF IMPERFECTIONS APPLIED DURING BUCKLING ANALYSIS OF CYLINDRICAL SHELL UNDER COMPRESSIVE LOAD
Original language description
Thin-walled structures like unstiffened cylindrical shells are prone to buckling. The imperfections, deviation from ideal shape, loading path or cutouts can considerably reduce buckling load of the structure. Three types of imperfections have been considered and compared ? geometrical imperfection represented by single perturbation load approach and two types of cutouts, the circular and the rectangular one. Abaqus standard software package have been used for analysis of cylindrical shells made from composite material.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
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Continuities
R - Projekt Ramcoveho programu EK
Others
Publication year
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
New Trends in Civil Aviation 2013
ISBN
978-80-7204-843-4
ISSN
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e-ISSN
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Number of pages
5
Pages from-to
63-67
Publisher name
Akademické nakladetelství CERM
Place of publication
Brno
Event location
University of Žilina
Event date
Jun 21, 2013
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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