Abstract The helicopter main rotor in forward flight is considered in this paper. The results for rigid blades and elastic blades are compared by the method of coupled simulation. The influence of the structural damping coefficient on the blade in-flight deformation is also considered.
Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight
Russian Aeronautics ; 60 , 2 ; 198-205
01.04.2017
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight
Online Contents | 2017
|British Library Conference Proceedings | 2011
|A LOOSELY COUPLED CFD/CSD SIMULATION OF A HELICOPTER ROTOR IN FORWARD FLIGHT
British Library Conference Proceedings | 2013
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