| Attributes | Values |
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| rdf:type
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| Description
| - Článek se zabývá porovnáním vypočtených aerodynamických charakteristik profilu MS 0313 bez a se štěrbinovou vztlakovou klapkou s experimentálními daty. Výpočty byly provedeny čtyřmi různými programy. Experimentální měření bylo provedeno ve VZLÚ a v NASA. Použité programy byly XFOIL, MSES, FLUENT a EDGE. Tyto programy používají tři různé metody výpočtu charakteristik proudového pole. XFOIL je založen na panelové metodě, MSES k výpočtu používá řešení Eulerových rovnic a FLUENT a EDGE řeší Navier-Stokesovy rovnice. Nastavení jednotlivých programů a charakter výpočtu bylo zkoumáno. Reynoldsovo číslo použité při výpočtu odpovídalo experimentu. Podařilo se dosáhnout velmi dobré shody mezi numerickými a experimentálními výsledky. (cs)
- The article describes computing results of the subsonic flow field around the airfoil MS 0313 with and without a slotted flap, computations obtained by four different CFD programs. These computational results have been compared with the experimental data carried out by experimental facilities of ARTI and NASA. The XFOIL, MSES, FLUENT and EDGE represent the programs used for the computation. These CFD programs use three different computational methods. XFOIL is based on panel methods, MSES is based on Euler equations and FLUENT and EDGE use Navier-Stokes equations as a base for numerical calculation using a simulation of intensity of turbulence. The specific set-up and character of each program and method have been investigated (e.g. the type and intensity of turbulence, the computational time and accuracy, the applications, etc.). The Reynolds number of Re = 2E6 corresponds to the airfoil without a slotted flap and Re = 1,76E6 corresponds to the airfoil with a slotted flap.
- The article describes computing results of the subsonic flow field around the airfoil MS 0313 with and without a slotted flap, computations obtained by four different CFD programs. These computational results have been compared with the experimental data carried out by experimental facilities of ARTI and NASA. The XFOIL, MSES, FLUENT and EDGE represent the programs used for the computation. These CFD programs use three different computational methods. XFOIL is based on panel methods, MSES is based on Euler equations and FLUENT and EDGE use Navier-Stokes equations as a base for numerical calculation using a simulation of intensity of turbulence. The specific set-up and character of each program and method have been investigated (e.g. the type and intensity of turbulence, the computational time and accuracy, the applications, etc.). The Reynolds number of Re = 2E6 corresponds to the airfoil without a slotted flap and Re = 1,76E6 corresponds to the airfoil with a slotted flap. (en)
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| Title
| - Comparison of Selected CFD Methods for the calculation of Aerodynamic Characteristics of the MS 0313 and MS 0317 Airfoils
- Comparison of Selected CFD Methods for the calculation of Aerodynamic Characteristics of the MS 0313 and MS 0317 Airfoils (en)
- Porovnání jednotlivých výpočtových metod pro výpočet aerodynamických charakteristik profilů MS 0313 a MS 0317 (cs)
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| skos:prefLabel
| - Comparison of Selected CFD Methods for the calculation of Aerodynamic Characteristics of the MS 0313 and MS 0317 Airfoils
- Comparison of Selected CFD Methods for the calculation of Aerodynamic Characteristics of the MS 0313 and MS 0317 Airfoils (en)
- Porovnání jednotlivých výpočtových metod pro výpočet aerodynamických charakteristik profilů MS 0313 a MS 0317 (cs)
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| skos:notation
| - RIV/68407700:21220/06:02134667!RIV08-MSM-21220___
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| http://linked.open.../vavai/riv/strany
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| http://linked.open...avai/riv/aktivita
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| http://linked.open...avai/riv/aktivity
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| http://linked.open...vai/riv/dodaniDat
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| http://linked.open...aciTvurceVysledku
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| http://linked.open.../riv/druhVysledku
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| http://linked.open...iv/duvernostUdaju
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| http://linked.open...titaPredkladatele
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| http://linked.open...dnocenehoVysledku
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| http://linked.open...ai/riv/idVysledku
| - RIV/68407700:21220/06:02134667
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| http://linked.open...riv/jazykVysledku
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| http://linked.open.../riv/klicovaSlova
| - Airfoils; CFD; comparison (en)
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| http://linked.open.../riv/klicoveSlovo
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| http://linked.open...ontrolniKodProRIV
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| http://linked.open...v/mistoKonaniAkce
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| http://linked.open...i/riv/mistoVydani
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| http://linked.open...i/riv/nazevZdroje
| - Advanced Engineering Design AED 2006
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| http://linked.open...in/vavai/riv/obor
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| http://linked.open...ichTvurcuVysledku
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| http://linked.open...cetTvurcuVysledku
| |
| http://linked.open...vavai/riv/projekt
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| http://linked.open...UplatneniVysledku
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| http://linked.open...iv/tvurceVysledku
| - Vrchota, Petr
- Anderle, P.
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| http://linked.open...vavai/riv/typAkce
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| http://linked.open.../riv/zahajeniAkce
| |
| number of pages
| |
| http://purl.org/ne...btex#hasPublisher
| - České vysoké učení technické v Praze
|
| https://schema.org/isbn
| |
| http://localhost/t...ganizacniJednotka
| |
| is http://linked.open...avai/riv/vysledek
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