A coupled rotor-fuselage aeroelastic analysis using complex rotor modes

0044 English OPEN
Chan, W.Y.;
  • Subject: TA

A new modal method capable of analysing the aeroelastic response of rotorcraft in both steady and manoeuvring flight is developed. Particular emphasis is given to the correct modelling of the dynamic interactions between the rotor and the fuselage. This is achieved via ... View more
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