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 in | Applied mathematics and mechanics Vol. 40; no. 8; pp. 1053 - 1082 |
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Main Authors | , , , , |
Format | Journal Article |
Language | English |
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 |
Edition | English ed. |
Subjects | |
Online Access | Get full text |
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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. |
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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 |
Author_xml | – sequence: 1 givenname: Jin surname: Zeng fullname: Zeng, Jin organization: School of Mechanical Engineering and Automation, Northeastern University – sequence: 2 givenname: Hui surname: Ma fullname: Ma, Hui email: huima@me.neu.edu.cn organization: School of Mechanical Engineering and Automation, Northeastern University, Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education, Northeastern University – sequence: 3 givenname: Kun surname: Yu fullname: Yu, Kun organization: School of Mechanical Engineering and Automation, Northeastern University – sequence: 4 givenname: Zhitao surname: Xu fullname: Xu, Zhitao organization: School of Mechanical Engineering and Automation, Northeastern University – sequence: 5 givenname: Bangchun surname: Wen fullname: Wen, Bangchun organization: School of Mechanical Engineering and Automation, Northeastern University |
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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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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 |
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