Rotor parameters of small weight helicopters

dc.contributor.author Dudnik, V.
dc.contributor.author Karabut, V.
dc.contributor.author Lesniak, S.
dc.date.accessioned 2024-04-17T10:38:32Z
dc.date.available 2024-04-17T10:38:32Z
dc.date.issued 2020
dc.description.abstract In recent years, a significant number of one and two-seats small weighted helicopters have appeared. This fact makes it possible to analyse the parameters and determine the parameter dependencies for this helicopters class. Knowledge of such dependencies is necessary for the preliminary design stage. The analysis performed in this paper and the comparison of it with the statistical data of all the categories of helicopters made it possible to determine the necessary corrections in the methods for design the parameters of the little helicopter's rotor systems.
dc.identifier.other 1516 erf2020
dc.identifier.uri https://hdl.handle.net/20.500.11881/4171
dc.language.iso en
dc.title Rotor parameters of small weight helicopters
Files
Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
1516 erf2020.pdf
Size:
598.35 KB
Format:
Adobe Portable Document Format
Description:
Collections