An assessment of the transient effect on helicopter main rotor stability and power demand

An assessment of the transient effect on helicopter main rotor stability and power demand

The researched object os a helicopter main rotor with blades of variable geometric twist characteristics. Variable torsion refers to systems of actuators made of shape memory alloys. The presented numerical analyses allow for evaluating both the dynamics of the rotor in transient states, i.e. in the...

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Bibliographic Details
Main Authors: Radosław Raczyński, Ksenia Siadkowska, Karol Ścisłowski, Mirosław Wendeker
Format: Article
Language:English
Published: Polskie Towarzystwo Naukowe Silników Spalinowych/Polish Scientific Society of Combustion Engines 2022-03-01
Series:Combustion Engines
Subjects:
helicopter
rotor
propulsion
power demand
transient effect
Online Access:http://www.combustion-engines.eu/An-assessment-of-the-transient-effect-on-helicopter-main-rotor-stability-and-power,146695,0,2.html

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http://www.combustion-engines.eu/An-assessment-of-the-transient-effect-on-helicopter-main-rotor-stability-and-power,146695,0,2.html

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