Open AccessMain rotor blade modeling approaches comparison. Finite element and Craig-Bampton methods
Author(s) -
В. І. Борисенко,
Jose Leoro,
Anton Didenko
Publication year - 2021
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/2131/3/032096
Subject(s) - blade (archaeology) , blade element theory , helicopter rotor , rotor (electric) , finite element method , aerodynamics , blade element momentum theory , action (physics) , basis (linear algebra) , structural engineering , amplitude , control theory (sociology) , computer science , engineering , mathematics , mechanics , physics , turbine blade , mechanical engineering , geometry , turbine , artificial intelligence , control (management) , quantum mechanics
The paper focuses on the helicopter main rotor blade FE model. And the main goal is to prove the feasibility of the helicopter main rotor MBD model in calculations of blade deformation as a result of applied aerodynamic forces. FE model is used as a basis for two different computational methods. A mathematical approach in the MBD based on the Craig-Bampton method on the one hand. And finite element model on the other hand. The results of high-frequency blade rotations are obtained. Calculations of these models are compared in order to determine the best method for modeling a linear-elastic blade. By the results, it is necessary to consider the preloaded state of the blade when using the Craig-Bampton method approach. The comparison of blade nodes displacements at various external conditions for both models are given. The influence of rotor MBS model damping parameters on the amplitude of blade oscillations under sinusoidal action is considered.