Measurement of aircraft propeller in yaw flow
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F17%3A00534130" target="_blank" >RIV/60162694:G43__/17:00534130 - isvavai.cz</a>
Result on the web
<a href="http://ieeexplore.ieee.org/document/7988821/" target="_blank" >http://ieeexplore.ieee.org/document/7988821/</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/MILTECHS.2017.7988821" target="_blank" >10.1109/MILTECHS.2017.7988821</a>
Alternative languages
Result language
angličtina
Original language name
Measurement of aircraft propeller in yaw flow
Original language description
This paper contents theory interpretation of a propeller in yaw and experimental results of tests to determine the thrust, power and efficiency characteristics of a propeller Bambula 18x8 at various angles of yaw from 0° to 90°. The results of the wind tunnel tests can contribute to completing the aerodynamic calculation of fixed-pitch propeller aircraft especially for multicopters, whose rotors are always operating in yaw flow.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20301 - Mechanical engineering
Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2017
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
International Conference on Military Technologies (ICMT), 2017
ISBN
978-1-5386-1988-9
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
566-569
Publisher name
Institute of Electrical and Electronics Engineers Inc.
Place of publication
Piscataway, NJ 08854-4141 USA
Event location
Brno
Event date
May 31, 2017
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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