Numerical simulation and mechanism research of flow-induced vibration of porous airfoils
The porous airfoil, inspired by avian wing morphology, exhibits complex flow-induced vibrations (FIVs) that significantly impact aerodynamic performance. This study employs computational fluid dynamics (CFD) methods to investigate FIV mechanisms of the porous airfoil through parametric analyses of a...
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Published in | Physics of fluids (1994) Vol. 37; no. 8 |
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01.08.2025
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Abstract | The porous airfoil, inspired by avian wing morphology, exhibits complex flow-induced vibrations (FIVs) that significantly impact aerodynamic performance. This study employs computational fluid dynamics (CFD) methods to investigate FIV mechanisms of the porous airfoil through parametric analyses of aspect ratio (AR), thickness ratio (TR), and additional sinusoidal motion in the wing. A high-fidelity CFD model is developed and validated against wind tunnel data, achieving errors within 10%. Key findings reveal: (1) non-monotonic lift variation with AR, peaking at
AR=6 due to suppressed vortex shedding; (2) linear reduction in lift coefficient with increasing TR, attributed to diminished pressure gradients; (3) periodic lift oscillations synchronized with sinusoidal motion, where shorter periods (0.1 s) induce stronger aerodynamic damping. The derived mechanisms provide guidelines for optimizing bio-inspired porous airfoils in applications requiring vibration suppression or energy harvesting. |
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AbstractList | The porous airfoil, inspired by avian wing morphology, exhibits complex flow-induced vibrations (FIVs) that significantly impact aerodynamic performance. This study employs computational fluid dynamics (CFD) methods to investigate FIV mechanisms of the porous airfoil through parametric analyses of aspect ratio (AR), thickness ratio (TR), and additional sinusoidal motion in the wing. A high-fidelity CFD model is developed and validated against wind tunnel data, achieving errors within 10%. Key findings reveal: (1) non-monotonic lift variation with AR, peaking at AR=6 due to suppressed vortex shedding; (2) linear reduction in lift coefficient with increasing TR, attributed to diminished pressure gradients; (3) periodic lift oscillations synchronized with sinusoidal motion, where shorter periods (0.1 s) induce stronger aerodynamic damping. The derived mechanisms provide guidelines for optimizing bio-inspired porous airfoils in applications requiring vibration suppression or energy harvesting. The porous airfoil, inspired by avian wing morphology, exhibits complex flow-induced vibrations (FIVs) that significantly impact aerodynamic performance. This study employs computational fluid dynamics (CFD) methods to investigate FIV mechanisms of the porous airfoil through parametric analyses of aspect ratio (AR), thickness ratio (TR), and additional sinusoidal motion in the wing. A high-fidelity CFD model is developed and validated against wind tunnel data, achieving errors within 10%. Key findings reveal: (1) non-monotonic lift variation with AR, peaking at AR=6 due to suppressed vortex shedding; (2) linear reduction in lift coefficient with increasing TR, attributed to diminished pressure gradients; (3) periodic lift oscillations synchronized with sinusoidal motion, where shorter periods (0.1 s) induce stronger aerodynamic damping. The derived mechanisms provide guidelines for optimizing bio-inspired porous airfoils in applications requiring vibration suppression or energy harvesting. |
Author | Ying, Changjie Guan, Guan Liang, Guopeng |
Author_xml | – sequence: 1 givenname: Changjie surname: Ying fullname: Ying, Changjie organization: School of Naval Architecture, Dalian University of Technology, Dalian 116024, China – sequence: 2 givenname: Guan surname: Guan fullname: Guan, Guan organization: School of Naval Architecture, Dalian University of Technology, Dalian 116024, China – sequence: 3 givenname: Guopeng surname: Liang fullname: Liang, Guopeng organization: School of Naval Architecture, Dalian University of Technology, Dalian 116024, China |
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Cites_doi | 10.1016/j.renene.2023.119133 10.1504/PCFD.2020.111397 10.1016/j.jsv.2023.117611 10.1016/j.ijheatmasstransfer.2023.124569 10.1016/j.energy.2023.128584 10.3390/su15010275 10.1007/s00707-018-2203-6 10.1016/j.jsv.2020.115574 10.1016/0017-9310(90)90015-M 10.1007/s11242-014-0397-1 10.1504/PCFD.2019.099598 10.1016/j.oceaneng.2024.118720 10.1016/j.oceaneng.2024.118314 10.2514/1.C037253 10.1016/j.euromechflu.2011.05.003 10.1007/BF02736231 10.1016/j.molliq.2016.11.022 10.1063/5.0153779 10.1063/5.0198034 10.1016/j.ijheatfluidflow.2009.12.009 10.1016/j.jfluidstructs.2023.103985 10.1016/j.oceaneng.2022.113613 10.1016/j.oceaneng.2023.115367 10.1063/5.0047512 |
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SubjectTerms | Aerodynamic coefficients Airfoils Aspect ratio Computational fluid dynamics Damping Energy harvesting Flow generated vibrations Pressure gradients Sine waves Thickness ratio Vibration control Vortex shedding Wind tunnels |
Title | Numerical simulation and mechanism research of flow-induced vibration of porous airfoils |
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