Aeroelasticity analysis of the wing UL-39
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F10%3A00169576" target="_blank" >RIV/68407700:21220/10:00169576 - 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
Aeroelasticity analysis of the wing UL-39
Original language description
This paper deals with computation of modal and flutter characteristic, investigating ailerons effectiveness and determine torsion divergence critical velocity at right half-wing of the aircraft UL-39.The problems are solved in FEM software MSC.Nastran.
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
<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)
Others
Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Studentská tvůrčí činnost 2010
ISBN
978-80-01-04533-6
ISSN
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e-ISSN
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Number of pages
15
Pages from-to
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Publisher name
ČVUT v Praze - Fakulta strojní
Place of publication
Praha
Event location
Praha
Event date
Mar 30, 2010
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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