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Published in 2020 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2020.06.074
Abstract: Abstract Aeromechanical instabilities arising due to frequency coalescence of different modes of a helicopter rotor and fuselage system is investigated. The focus is on removing the small angle approximation typically used for ground resonance analysis…
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Keywords:
ground;
analysis;
ground resonance;
rotor fuselage ... See more keywords