Ruckling and Failure of Composite Web

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F02%3APU31517" target="_blank" >RIV/00216305:26210/02:PU31517 - 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
Ruckling and Failure of Composite Web
Original language description
Laboratory of aircraft technology of the Institute of Aerospace Engineering has been gradually gained some experience in the field of testing and behaviour of the composite aircraft wing structures. The latest test was the wing of the successful ultralight aircraft TL ? 2000 Carbon Sting. The tests and measurements, done with this wing, should have helped to evaluate and compare the root part of the wing structure, i.e. the root part of the beam in front of and behind the root rib, the typical web parrts of the root rib and the parts of root web under the point of application of local force.
Czech name
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Czech description
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Project
<a href="/en/project/LN00B051" target="_blank" >LN00B051: Aerospace research centre (ARC)</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2002
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
Fifth International Seminar on RECENT RESEARCH AND DESIGN PROGRESS IN AERONAUTICAL ENGINEERING AND INFLUENCE ON EDUCATION, Book of Abstracts
ISBN
9986-05-571-7
ISSN
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e-ISSN
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Number of pages
1
Pages from-to
54-54
Publisher name
VGTU
Place of publication
Vilnius, Lithuania
Event location
Vilnius
Event date
Nov 27, 2002
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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