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Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight
Authors:F Dehaeze  G N Barakos  L I Garipova  A N Kusyumov  S A Mikhailov
Institution:1.University of Liverpool,Liverpool,UK;2.University of Glasgow,Glasgow,Scotland, UK;3.Tupolev Kazan National Research Technical University,Kazan,Russia
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.
Keywords:
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