Development of three-dimensional co-rotational beam model for nonlinear dynamic analysis of highly flexible slender composite blades
The main purpose of this work is to introduce a novel method analyzing the dynamic response of a highly flexible slender composite beam having anisotropic property and variable cross-section. A three-dimensional co-rotational model is developed. The beam deformation in dynamic conditions is obtained...
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rr-article-197015442022-03-26T00:00:00Z Development of three-dimensional co-rotational beam model for nonlinear dynamic analysis of highly flexible slender composite blades Hyeongmin Moon (8064818) Haeseong Cho (12495499) Stephanos Theodossiades (1247457) Taeseong Kim (5516717) nonlinear dynamics 3D co-rotational method anisotropic beam highly flexible slender beam time domain analysis The main purpose of this work is to introduce a novel method analyzing the dynamic response of a highly flexible slender composite beam having anisotropic property and variable cross-section. A three-dimensional co-rotational model is developed. The beam deformation in dynamic conditions is obtained by applying HHT-α method as dynamic analysis tool. Validation studies with various boundary conditions, multiple external loads and pre-curved structures are performed. Furthermore, dynamic analysis with a large, flexible, and slender composite blade is performed with and without structural couplings. It is shown the developed beam model accurately predicts nonlinear three-dimensional response and anisotropic structural coupling effects. 2022-03-26T00:00:00Z Text Journal contribution 2134/19701544.v1 https://figshare.com/articles/journal_contribution/Development_of_three-dimensional_co-rotational_beam_model_for_nonlinear_dynamic_analysis_of_highly_flexible_slender_composite_blades/19701544 CC BY-NC 4.0 |
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nonlinear dynamics 3D co-rotational method anisotropic beam highly flexible slender beam time domain analysis |
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nonlinear dynamics 3D co-rotational method anisotropic beam highly flexible slender beam time domain analysis Hyeongmin Moon Haeseong Cho Stephanos Theodossiades Taeseong Kim Development of three-dimensional co-rotational beam model for nonlinear dynamic analysis of highly flexible slender composite blades |
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The main purpose of this work is to introduce a novel method analyzing the dynamic response of a highly flexible slender composite beam having anisotropic property and variable cross-section. A three-dimensional co-rotational model is developed. The beam deformation in dynamic conditions is obtained by applying HHT-α method as dynamic analysis tool. Validation studies with various boundary conditions, multiple external loads and pre-curved structures are performed. Furthermore, dynamic analysis with a large, flexible, and slender composite blade is performed with and without structural couplings. It is shown the developed beam model accurately predicts nonlinear three-dimensional response and anisotropic structural coupling effects. |
format |
Default Article |
author |
Hyeongmin Moon Haeseong Cho Stephanos Theodossiades Taeseong Kim |
author_facet |
Hyeongmin Moon Haeseong Cho Stephanos Theodossiades Taeseong Kim |
author_sort |
Hyeongmin Moon (8064818) |
title |
Development of three-dimensional co-rotational beam model for nonlinear dynamic analysis of highly flexible slender composite blades |
title_short |
Development of three-dimensional co-rotational beam model for nonlinear dynamic analysis of highly flexible slender composite blades |
title_full |
Development of three-dimensional co-rotational beam model for nonlinear dynamic analysis of highly flexible slender composite blades |
title_fullStr |
Development of three-dimensional co-rotational beam model for nonlinear dynamic analysis of highly flexible slender composite blades |
title_full_unstemmed |
Development of three-dimensional co-rotational beam model for nonlinear dynamic analysis of highly flexible slender composite blades |
title_sort |
development of three-dimensional co-rotational beam model for nonlinear dynamic analysis of highly flexible slender composite blades |
publishDate |
2022 |
url |
https://hdl.handle.net/2134/19701544.v1 |
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1797457784227233792 |