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Published in 2019 at "CEAS Aeronautical Journal"
DOI: 10.1007/s13272-019-00395-0
Abstract: Structural couplings between the flexible main rotor and the flexible drivetrain of the Bo105 helicopter are investigated by numerical simulation. For this purpose, the rotor hub constraint $$\varOmega ={\text {const.}}$$ Ω = const. is dropped…
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Keywords:
rotor;
drivetrain;
lag modes;
helicopter ... See more keywords