Coupled flapwise-chordwise-axial-torsional dynamic responses of rotating pre-twisted and inclined cantilever beams subject to the base excitation

A rotating pre-twisted and inclined cantilever beam model (RPICBM) with the flapwise-chordwise-axial-torsional coupling is established with the Hamilton principle and the finite element (FE) method. The effectiveness of the model is verified via comparisons with the literatures and the FE models in...

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Published inApplied mathematics and mechanics Vol. 40; no. 8; pp. 1053 - 1082
Main Authors Zeng, Jin, Ma, Hui, Yu, Kun, Xu, Zhitao, Wen, Bangchun
Format Journal Article
LanguageEnglish
Published Shanghai Shanghai University 01.08.2019
Springer Nature B.V
School of Mechanical Engineering and Automation, Northeastern University,Shenyang 110819, China%School of Mechanical Engineering and Automation, Northeastern University,Shenyang 110819, China
Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education, Northeastern University, Shenyang 110819, China
EditionEnglish ed.
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Abstract A rotating pre-twisted and inclined cantilever beam model (RPICBM) with the flapwise-chordwise-axial-torsional coupling is established with the Hamilton principle and the finite element (FE) method. The effectiveness of the model is verified via comparisons with the literatures and the FE models in ANSYS. The effects of the setting and pre-twisted angles on the dynamic responses of the RPICBM are analyzed. The results show that: (i) the increase in the setting or pre-twisted angle results in the increases in the first-order flapwise and torsional frequencies while the decrease in the first-order chordwise frequency under rotating conditions; (ii) a positive/negative setting angle leads to a positive/negative constant component, while a positive/negative pre-twisted angle leads to a negative/positive constant component; (iii) when the rotation speed is non-zero, the pre-twisted angle or non-zero setting angle will result in the coupled flapwise-chordwise-axial-torsional vibration of the RPICBM under axial base excitation.
AbstractList A rotating pre-twisted and inclined cantilever beam model (RPICBM) with the flapwise-chordwise-axial-torsional coupling is established with the Hamilton principle and the finite element (FE) method. The effectiveness of the model is verified via comparisons with the literatures and the FE models in ANSYS. The effects of the setting and pre-twisted angles on the dynamic responses of the RPICBM are analyzed. The results show that: (i) the increase in the setting or pre-twisted angle results in the increases in the first-order flapwise and torsional frequencies while the decrease in the first-order chordwise frequency under rotating conditions; (ii) a positive/negative setting angle leads to a positive/negative constant component, while a positive/negative pre-twisted angle leads to a negative/positive constant component; (iii) when the rotation speed is non-zero, the pre-twisted angle or non-zero setting angle will result in the coupled flapwise-chordwise-axial-torsional vibration of the RPICBM under axial base excitation.
O347.6%V214.3+7; A rotating pre-twisted and inclined cantilever beam model (RPICBM) with the flapwise-chordwise-axial-torsional coupling is established with the Hamilton principle and the finite element (FE) method.The effectiveness of the model is verified via comparisons with the literatures and the FE models in ANSYS.The effects of the setting and pre-twisted angles on the dynamic responses of the RPICBM are analyzed.The results show that:(ⅰ) the increase in the setting or pre-twisted angle results in the increases in the first-order flapwise and torsional frequencies while the decrease in the first-order chordwise frequency under rotating conditions;(ⅱ) a positive/negative setting angle leads to a positive/negative constant component,while a positive/negative pre-twisted angle leads to a negative/positive constant component;(ⅲ) when the rotation speed is non-zero,the pre-twisted angle or non-zero setting angle will result in the coupled flapwise-chordwise-axial-torsional vibration of the RPICBM under axial base excitation.
Author Yu, Kun
Wen, Bangchun
Zeng, Jin
Ma, Hui
Xu, Zhitao
AuthorAffiliation School of Mechanical Engineering and Automation, Northeastern University,Shenyang 110819, China%School of Mechanical Engineering and Automation, Northeastern University,Shenyang 110819, China;Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education, Northeastern University, Shenyang 110819, China
AuthorAffiliation_xml – name: School of Mechanical Engineering and Automation, Northeastern University,Shenyang 110819, China%School of Mechanical Engineering and Automation, Northeastern University,Shenyang 110819, China;Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education, Northeastern University, Shenyang 110819, China
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Issue 8
Keywords modal characteristic
flapwise-chordwise-axial-torsional
65L15
74S05
rotating Timoshenko beam
vibration response
7
base excitation
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Snippet A rotating pre-twisted and inclined cantilever beam model (RPICBM) with the flapwise-chordwise-axial-torsional coupling is established with the Hamilton...
O347.6%V214.3+7; A rotating pre-twisted and inclined cantilever beam model (RPICBM) with the flapwise-chordwise-axial-torsional coupling is established with...
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proquest
crossref
springer
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SubjectTerms Applications of Mathematics
Cantilever beams
Classical Mechanics
Excitation
Finite element method
Fluid- and Aerodynamics
Hamilton's principle
Mathematical Modeling and Industrial Mathematics
Mathematics
Mathematics and Statistics
Partial Differential Equations
Rotation
Torsion
Torsional vibration
Title Coupled flapwise-chordwise-axial-torsional dynamic responses of rotating pre-twisted and inclined cantilever beams subject to the base excitation
URI https://link.springer.com/article/10.1007/s10483-019-2506-6
https://www.proquest.com/docview/2266403679
https://d.wanfangdata.com.cn/periodical/yysxhlx-e201908001
Volume 40
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