Sign Up to like & get
recommendations!
0
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…
read more here.
Keywords:
ground;
analysis;
ground resonance;
rotor fuselage ... See more keywords
Sign Up to like & get
recommendations!
0
Published in 2017 at "Applied Sciences"
DOI: 10.3390/app7090918
Abstract: In this work, fully-resolved rotor-fuselage interactional aerodynamics is used as the forcing term in a model based on the Euler-Bernoulli equation, aiming to simulate helicopter tail-boom vibration. The model is based on linear beam analysis…
read more here.
Keywords:
computational fluid;
fluid dynamics;
boom;
tail boom ... See more keywords