About: On Numerical Approximation of Airfoil Vibrations after Loosing of Aeroelastic Stability     Goto   Sponge   NotDistinct   Permalink

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  • This paper describes the numerical approximation of flow around flexibly supported NACA 0012 airfoil with rotating aileron. The motion of the airfoil is described with the aid of system of ordinary differential equations (ODE) for three degrees of freedom coupled with the Navier-Stokes system of equations. The flow problem is approximated with the aid of stabilized finite element method and strongly coupled with solution of the system of ODEs. Numerical results are presented.
  • This paper describes the numerical approximation of flow around flexibly supported NACA 0012 airfoil with rotating aileron. The motion of the airfoil is described with the aid of system of ordinary differential equations (ODE) for three degrees of freedom coupled with the Navier-Stokes system of equations. The flow problem is approximated with the aid of stabilized finite element method and strongly coupled with solution of the system of ODEs. Numerical results are presented. (en)
Title
  • On Numerical Approximation of Airfoil Vibrations after Loosing of Aeroelastic Stability
  • On Numerical Approximation of Airfoil Vibrations after Loosing of Aeroelastic Stability (en)
skos:prefLabel
  • On Numerical Approximation of Airfoil Vibrations after Loosing of Aeroelastic Stability
  • On Numerical Approximation of Airfoil Vibrations after Loosing of Aeroelastic Stability (en)
skos:notation
  • RIV/68407700:21220/11:00183352!RIV12-MSM-21220___
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  • P(GAP101/11/0207), Z(MSM6840770003)
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  • 218086
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  • RIV/68407700:21220/11:00183352
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  • aeroelasticity; finite element method (en)
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  • [0443B2428746]
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  • Halkidiki
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  • Melville, New York
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  • ICNAAM-2011 Proceedings of the International Conference on Numerical Analysis and Applied Mathematics 2011
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  • Sváček, Petr
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number of pages
http://bibframe.org/vocab/doi
  • 10.1063/1.3636679
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  • American Institute of Physics
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  • 978-0-7354-0954-5
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  • 21220
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