Adaptation of main rotor of small helicopter at different altitudes

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F19%3A00537402" target="_blank" >RIV/60162694:G43__/19:00537402 - isvavai.cz</a>
Result on the web
<a href="http://ieeexplore.ieee.org/xpl/mostRecentIssue.jsp?punumber=8863088" target="_blank" >http://ieeexplore.ieee.org/xpl/mostRecentIssue.jsp?punumber=8863088</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/MILTECHS.2019.8870110" target="_blank" >10.1109/MILTECHS.2019.8870110</a>

Result language
angličtina
Original language name
Adaptation of main rotor of small helicopter at different altitudes
Original language description
This paper presents a discussion to some results of the calculation and measurement of aerodynamic characteristics of helicopter in the hover. A simple blade element model (BEM) is presented and a calculation of flight performance in a hover of helicopter Mikado L O G O 600 3D in various altitudes was performed as well. Results of the calculation are compared to the measurement conducted in the wind tunnel.
Czech name
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Czech description
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Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
ICMT 2019 - 7th International Conference on Military Technologies, Proceedings
ISBN
978-1-7281-4593-8
ISSN
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e-ISSN
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Number of pages
5
Pages from-to
1-5
Publisher name
Institute of Electrical and Electronics Engineers Inc.
Place of publication
Piscataway, USA
Event location
Brno, the Czech Republic
Event date
May 30, 2019
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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