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  • The fluid structure interaction (FSI) represents an important task in many applications. This paper deals with interaction of airfoil and fluid flow and compares two possible ways of computation of the stability boundaries of the system. The airfoil has two degrees of freedom represented by translation h(t) and rotation a(t). The flow acts on the airfoil with aerodynamic forces depending on the flow velocity. Two methods for calculation of the critical flow velocity, when the airfoil loses aeroleastic stability, are described.
  • The fluid structure interaction (FSI) represents an important task in many applications. This paper deals with interaction of airfoil and fluid flow and compares two possible ways of computation of the stability boundaries of the system. The airfoil has two degrees of freedom represented by translation h(t) and rotation a(t). The flow acts on the airfoil with aerodynamic forces depending on the flow velocity. Two methods for calculation of the critical flow velocity, when the airfoil loses aeroleastic stability, are described. (en)
Title
  • Analytical and numerical approach to the airfoil stability computation
  • Analytical and numerical approach to the airfoil stability computation (en)
skos:prefLabel
  • Analytical and numerical approach to the airfoil stability computation
  • Analytical and numerical approach to the airfoil stability computation (en)
skos:notation
  • RIV/61388998:_____/13:00421337!RIV14-GA0-61388998
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  • I, P(GAP101/11/0207)
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  • 60761
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  • RIV/61388998:_____/13:00421337
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  • aeroelasticity; flutter; boundary of stability (en)
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  • [BB573A37CE59]
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  • Praha
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  • Praha
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  • Colloquium FLUID DYNAMICS 2013
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  • Horáček, Jaromír
  • Chládek, Štěpán
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number of pages
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  • Ústav termomechaniky AV ČR
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  • 978-80-87012-48-2
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