Computation of static deformations of elastic wing
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F12%3A%230001461" target="_blank" >RIV/00010669:_____/12:#0001461 - isvavai.cz</a>
Result on the web
<a href="http://www.czaerospace.eu/en/2012-02-44.html" target="_blank" >http://www.czaerospace.eu/en/2012-02-44.html</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Computation of static deformations of elastic wing
Original language description
A method of computation of static torsional and bending deformations of an elastic wing due to aerodynamic, elastic and gravitational forces is described. A wing in elastic model is represented by elastic axis with defined elasticity and by distributionof mass. Aerodynamic forces acting on the wing are computed using non-linearized airfoil aerodynamic characteristics.
Czech name
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Czech description
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Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2012
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Czech Aerospace Proceedings / Letecký zpravodaj
ISSN
1211-877X
e-ISSN
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Volume of the periodical
2/2012
Issue of the periodical within the volume
2
Country of publishing house
CZ - CZECH REPUBLIC
Number of pages
3
Pages from-to
9 - 11
UT code for WoS article
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EID of the result in the Scopus database
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