Determination of the Energy Performance of a Helicopter in a Hover

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F18%3A00536596" target="_blank" >RIV/60162694:G43__/18:00536596 - isvavai.cz</a>
Result on the web
<a href="http://www.engmech.cz/im/proceedings/show_p/2018/121" target="_blank" >http://www.engmech.cz/im/proceedings/show_p/2018/121</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.21495/91-8-121" target="_blank" >10.21495/91-8-121</a>

Result language
angličtina
Original language name
Determination of the Energy Performance of a Helicopter in a Hover
Original language description
This paper deals with the calculation and measurement of aerodynamic characteristics in the hover of a radio-controlled helicopter. After a brief introduction of the efficiency and adaptation conditions of the rotors, the article focuses on the determination of the power envelope and specific power of the helicopter propulsion unit. The main purpose is to familiarize the reader with the calculation of the energy intensity of the helicopter in the hover and its verification by laboratory measurement. The calculation is done by using the ideal propulsion theory and simplified blade element theory. The final discussion focuses on the determination of the energy performance of a helicopter in a hover.
Czech name
—
Czech description
—

Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
ENGINEERING MECHANICS 2018
ISBN
978-80-86246-88-8
ISSN
1805-8248
e-ISSN
1805-8256
Number of pages
4
Pages from-to
121-124
Publisher name
Institute of Theoretical and Applied Mechanics of the Cech Academy of Sciences
Place of publication
Prague
Event location
Svratka
Event date
May 14, 2018
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
000465489800030

Similar results(10)