Finite Element Framework for Efficient Design of Three Dimensional Multicomponent Composite Helicopter Rotor Blade System
In the present study, a three-dimensional finite element framework has been developed to model a full-scale multilaminate composite helicopter rotor blade. Tip deformation and stress behavior have been analyzed for external aerodynamic loading conditions and compared with the Abaqus FEA model. Furth...
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| Format: | Article |
| Language: | English |
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MDPI AG
2021-03-01
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| Series: | Eng |
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| Online Access: | https://www.mdpi.com/2673-4117/2/1/6 |