. . "RIV/68407700:21220/10:00174738" . . . "Pr\u00E1ce se zab\u00FDv\u00E1 numerick\u00FDm modelov\u00E1n\u00EDm lamin\u00E1rn\u00EDho a turbulentn\u00EDho obt\u00E9k\u00E1n\u00ED \u0161\u00EDpov\u00E9ho k\u0159\u00EDdla ve vn\u011Bj\u0161\u00ED aerodynamice. V\u00FDchoz\u00ED syst\u00E9m Navierov\u00FDch-Stokesov\u00FDch rovnic s Reynoldsov\u00FDm st\u0159edov\u00E1n\u00EDm je \u0159e\u0161en pomoc\u00ED metody kone\u010Dn\u00FDch objem\u016F ve form\u011B cell-centered. Jmenovit\u011B pak tzv. Modifikovan\u00FDm Causonov\u00FDm sch\u00E9matem (MCS, pou\u017Eito pouze pro lamin\u00E1rn\u00ED v\u00FDpo\u010Det) a WLSQR sch\u00E9matem s HLLC numerick\u00FDm tokem (turbulentn\u00ED v\u00FDpo\u010Det). Turbulentn\u00ED jevy jsou simulov\u00E1ny pomoc\u00ED dvou r\u016Fzn\u00FDch model\u016F turbulence a to sice Kokova TNT modelu a Spalartova-Allmarasova modelu. Z\u00EDskan\u00E9 v\u00FDsledky jsou srovn\u00E1ny s experiment\u00E1ln\u00EDmi daty s velice dobrou shodou. Lamin\u00E1rn\u00ED v\u00FDsledky z\u00EDskan\u00E9 pomoc\u00ED MCS sch\u00E9matu jsou sice pouze p\u0159edb\u011B\u017En\u00E9, ale ukazuj\u00ED na schopnost sch\u00E9matu \u0159e\u0161it slo\u017Eit\u011Bj\u0161\u00ED p\u0159\u00EDpady proud\u011Bn\u00ED." . "Numerical Simulation of Turbulent Flow ower a Swept Wing"@en . . "5" . . . "FVM; TVD; WLSQR; TNT Kok; SST; turbulence; transonic flow"@en . . "Numerical Simulation of Turbulent Flow ower a Swept Wing"@en . "Pr\u00E1ce se zab\u00FDv\u00E1 numerick\u00FDm modelov\u00E1n\u00EDm lamin\u00E1rn\u00EDho a turbulentn\u00EDho obt\u00E9k\u00E1n\u00ED \u0161\u00EDpov\u00E9ho k\u0159\u00EDdla ve vn\u011Bj\u0161\u00ED aerodynamice. V\u00FDchoz\u00ED syst\u00E9m Navierov\u00FDch-Stokesov\u00FDch rovnic s Reynoldsov\u00FDm st\u0159edov\u00E1n\u00EDm je \u0159e\u0161en pomoc\u00ED metody kone\u010Dn\u00FDch objem\u016F ve form\u011B cell-centered. Jmenovit\u011B pak tzv. Modifikovan\u00FDm Causonov\u00FDm sch\u00E9matem (MCS, pou\u017Eito pouze pro lamin\u00E1rn\u00ED v\u00FDpo\u010Det) a WLSQR sch\u00E9matem s HLLC numerick\u00FDm tokem (turbulentn\u00ED v\u00FDpo\u010Det). Turbulentn\u00ED jevy jsou simulov\u00E1ny pomoc\u00ED dvou r\u016Fzn\u00FDch model\u016F turbulence a to sice Kokova TNT modelu a Spalartova-Allmarasova modelu. Z\u00EDskan\u00E9 v\u00FDsledky jsou srovn\u00E1ny s experiment\u00E1ln\u00EDmi daty s velice dobrou shodou. Lamin\u00E1rn\u00ED v\u00FDsledky z\u00EDskan\u00E9 pomoc\u00ED MCS sch\u00E9matu jsou sice pouze p\u0159edb\u011B\u017En\u00E9, ale ukazuj\u00ED na schopnost sch\u00E9matu \u0159e\u0161it slo\u017Eit\u011Bj\u0161\u00ED p\u0159\u00EDpady proud\u011Bn\u00ED."@cs . "CZ - \u010Cesk\u00E1 republika" . "[1A903AC92415]" . "1801-9315" . "275700" . "Kozel, Karel" . "Numerick\u00E1 simulace turbulentn\u00EDho obt\u00E9k\u00E1n\u00ED \u0161\u00EDpov\u00E9ho k\u0159\u00EDdla" . "12" . "F\u00FCrst, Ji\u0159\u00ED" . "8"^^ . "P(GA101/07/1508), Z(MSM6840770010)" . . "Furm\u00E1nek, Petr" . . "Numerick\u00E1 simulace turbulentn\u00EDho obt\u00E9k\u00E1n\u00ED \u0161\u00EDpov\u00E9ho k\u0159\u00EDdla"@cs . . . "Numerick\u00E1 simulace turbulentn\u00EDho obt\u00E9k\u00E1n\u00ED \u0161\u00EDpov\u00E9ho k\u0159\u00EDdla" . "21220" . . . . "This work deals with numerical modelling of laminar and turbulent flow over an swept wing. As the governing system of equation the system of Reynolds averaged Navier-Stokes equations was chosen. Numerical solution was realized by two diferent cell-centered schemes of the finite volume method, namely the Modified Causon's scheme and WLSQR scheme with HLLC numerical flux. Turbulence effects are simulated by two models of turbulence - the Kok's TNT model and Spalart-Allmaras model. Obtained results are compared with experimental data with a very good agreement. Results obtained for te case of laminar flow are only preliminary, but they show all the characteristics as expected."@en . . "Transfer - V\u00FDzkum a v\u00FDvoj pro leteck\u00FD pr\u016Fmysl" . . . "1"^^ . . . "Numerick\u00E1 simulace turbulentn\u00EDho obt\u00E9k\u00E1n\u00ED \u0161\u00EDpov\u00E9ho k\u0159\u00EDdla"@cs . . "RIV/68407700:21220/10:00174738!RIV11-GA0-21220___" . "3"^^ .