Effect of the wing shape on the thrust of flapping wing
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216208%3A11320%2F11%3A10108870" target="_blank" >RIV/00216208:11320/11:10108870 - isvavai.cz</a>
Result on the web
<a href="http://dx.doi.org/10.1016/j.apm.2011.04.003" target="_blank" >http://dx.doi.org/10.1016/j.apm.2011.04.003</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1016/j.apm.2011.04.003" target="_blank" >10.1016/j.apm.2011.04.003</a>
Alternative languages
Result language
angličtina
Original language name
Effect of the wing shape on the thrust of flapping wing
Original language description
Simulations of harmonically oscillating wings were performed using two-dimensional and three-dimensional boundary element method computer programs: the corresponding hydrodynamic forces were obtained by assuming potential flow.
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
BK - Liquid mechanics
OECD FORD branch
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Result continuities
Project
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Continuities
V - Vyzkumna aktivita podporovana z jinych verejnych zdroju
Others
Publication year
2011
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Applied Mathematical Modelling
ISSN
0307-904X
e-ISSN
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Volume of the periodical
2011/35
Issue of the periodical within the volume
10
Country of publishing house
NL - THE KINGDOM OF THE NETHERLANDS
Number of pages
12
Pages from-to
4979-4990
UT code for WoS article
000292176200024
EID of the result in the Scopus database
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