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  • This work deals with numerical solution of transonic flow past a 2D profile (steady viscous turbulent flow) and a 3D swept wing (steady inviscid flow). In this work we use several types of finite volume schemes. Firstly explicit schemes based on Lax-Wendroff type schemes in the cellcentered (MacCormack) and cell-vertex (Ron-Ho-Ni) form are used. For 2D steady and turbulent flows over RAE 2822 authors used implicit scheme based on modern ENO and ROE schemes. For all computational results authors used solver developed at our department and in Aeronautical Research and Test Institute in Prague Letnany during long term research work in this field.
  • This work deals with numerical solution of transonic flow past a 2D profile (steady viscous turbulent flow) and a 3D swept wing (steady inviscid flow). In this work we use several types of finite volume schemes. Firstly explicit schemes based on Lax-Wendroff type schemes in the cellcentered (MacCormack) and cell-vertex (Ron-Ho-Ni) form are used. For 2D steady and turbulent flows over RAE 2822 authors used implicit scheme based on modern ENO and ROE schemes. For all computational results authors used solver developed at our department and in Aeronautical Research and Test Institute in Prague Letnany during long term research work in this field. (en)
  • Práce se zabývá numerickým řešením transsonického proudění okolo profilu (2D, stacionární vazký turbulentní model) a šípového křídla (3D, stacionární nevazký model). Pro řešení je použito více typů schémat metody konečných objemů. V trojrozměrném případě jsou jako první uvedena schémata typu Laxe-Wendroffa jak ve formě cell-centered (MacCormackovo schéma), tak ve formě cell-vertex (Ron-Ho-Ni). Pro dvourozměrný případ turbulentního obtékání profilu RAE 2822 byla použita implicitní schémata založená na ENO a ROE schématech. Všechny použité programy byly vyvinuty na našem pracovišti a ve Výzkumném a zkušebním leteckém ústavu v rámci dlouhodobé výzkumné práce. (cs)
Title
  • Numerical Solution of Transonic Flows over an Airfoil and a Wing
  • Numerické řešení transsonického proudění okolo profilu a křídla (cs)
  • Numerical Solution of Transonic Flows over an Airfoil and a Wing (en)
skos:prefLabel
  • Numerical Solution of Transonic Flows over an Airfoil and a Wing
  • Numerické řešení transsonického proudění okolo profilu a křídla (cs)
  • Numerical Solution of Transonic Flows over an Airfoil and a Wing (en)
skos:notation
  • RIV/68407700:21220/06:02121728!RIV07-MSM-21220___
http://linked.open...avai/riv/aktivita
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  • Z(MSM6840770010)
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  • 489411
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  • RIV/68407700:21220/06:02121728
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  • Euler equations; RANS; cell-centered scheme; cell-vertex scheme; transonic flows; turbulence modelling (en)
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  • [C6F55AFD067D]
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  • Budapest
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  • neuvedeno
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  • Furmánek, Petr
  • Fürst, Jiří
  • Kozel, Karel
  • Dobeš, Jiří
  • Fořt, Jaroslav
  • Kladrubský, Milan
http://linked.open...n/vavai/riv/zamer
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  • 963-420-872-X
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  • 21220
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