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Description
  • During the last few years, unsteady and aeroelastic simulations have become a standard part of CFD computations in aeronautical applications. They are usually used with various types of turbulent models the most of which are derived from system of the Reynolds-Averaged Navier–Stokes equations (RANS). However, the RANS system itself is derived using time-averaging and hence it neglects certain type of unsteadiness in its own nature. Therefore it is necessary to investigate what is the ability of the contemporary numerical methods (i.e. combinations of numerical schemes and turbulence models) to simulate various types of unsteady flows. The authors carried out a series of numerical tests of two types of unsteady flows in external aerodynamics. Namely the transonic compressible flow over harmonically oscillating NACA 0012 aerofoil and subsonic compressible flow over the same aerofoil with oscillations induced by the flow itself (i.e. considering the aeroelastic interaction). Three different high-order finite volume schemes with various contemporary turbulence models were chosen for the testing.
  • During the last few years, unsteady and aeroelastic simulations have become a standard part of CFD computations in aeronautical applications. They are usually used with various types of turbulent models the most of which are derived from system of the Reynolds-Averaged Navier–Stokes equations (RANS). However, the RANS system itself is derived using time-averaging and hence it neglects certain type of unsteadiness in its own nature. Therefore it is necessary to investigate what is the ability of the contemporary numerical methods (i.e. combinations of numerical schemes and turbulence models) to simulate various types of unsteady flows. The authors carried out a series of numerical tests of two types of unsteady flows in external aerodynamics. Namely the transonic compressible flow over harmonically oscillating NACA 0012 aerofoil and subsonic compressible flow over the same aerofoil with oscillations induced by the flow itself (i.e. considering the aeroelastic interaction). Three different high-order finite volume schemes with various contemporary turbulence models were chosen for the testing. (en)
Title
  • Deterministic unsteady and aeroelastic flow simulations with high-order FVM schemes
  • Deterministic unsteady and aeroelastic flow simulations with high-order FVM schemes (en)
skos:prefLabel
  • Deterministic unsteady and aeroelastic flow simulations with high-order FVM schemes
  • Deterministic unsteady and aeroelastic flow simulations with high-order FVM schemes (en)
skos:notation
  • RIV/68407700:21220/13:00226695!RIV15-GA0-21220___
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(GAP101/11/0207)
http://linked.open...iv/cisloPeriodika
  • January
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  • 68987
http://linked.open...ai/riv/idVysledku
  • RIV/68407700:21220/13:00226695
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • ALE; EARSM; FVM; Jameson’s AD; Kok’s TNT, Spalart–Allmaras; Unsteady flow (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...odStatuVydavatele
  • DE - Spolková republika Německo
http://linked.open...ontrolniKodProRIV
  • [5E777AE56D51]
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  • Computing
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http://linked.open...UplatneniVysledku
http://linked.open...v/svazekPeriodika
  • 95
http://linked.open...iv/tvurceVysledku
  • Furmánek, Petr
  • Kozel, Karel
http://linked.open...ain/vavai/riv/wos
  • 000338630100011
issn
  • 0010-485X
number of pages
http://bibframe.org/vocab/doi
  • 10.1007/s00607-013-0291-7
http://localhost/t...ganizacniJednotka
  • 21220
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