Aerodynamic Efficiency Optimization of Clark Y Aerofoil Using SU2 Application

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F70883521%3A28140%2F16%3A43874303" target="_blank" >RIV/70883521:28140/16:43874303 - isvavai.cz</a>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Aerodynamic Efficiency Optimization of Clark Y Aerofoil Using SU2 Application

Popis výsledku v původním jazyce

In this paper, the aerodynamic efficiency optimizations of the Clark Y aerofoil by using the SU2 software suite are performed. We used a low-speed inviscid flow with the Mach number of approximately 0.0441 (15 m/s) for the optimization. To determine whether we found completely optimized aerofoils, we had to analyse the optimized aerofoils at surrounding angles of attack after the optimization. Moreover, we extended the analysis to obtain information whether the aerofoils can also be effectively used at higher velocities (up to 30 m/s). We executed and analysed five optimizations with the different number of design variables: 8, 18, 38, 78, and 158. Firstly, the aerodynamics of aerofoil is briefly described and the most important parameters are explained. In the following section, the SU2 software used for the optimizations is outlined and the optimization method is introduced. Finally, the results of the efficiency optimizations are presented, compared, and analysed.

Název v anglickém jazyce

Aerodynamic Efficiency Optimization of Clark Y Aerofoil Using SU2 Application

Popis výsledku anglicky

In this paper, the aerodynamic efficiency optimizations of the Clark Y aerofoil by using the SU2 software suite are performed. We used a low-speed inviscid flow with the Mach number of approximately 0.0441 (15 m/s) for the optimization. To determine whether we found completely optimized aerofoils, we had to analyse the optimized aerofoils at surrounding angles of attack after the optimization. Moreover, we extended the analysis to obtain information whether the aerofoils can also be effectively used at higher velocities (up to 30 m/s). We executed and analysed five optimizations with the different number of design variables: 8, 18, 38, 78, and 158. Firstly, the aerodynamics of aerofoil is briefly described and the most important parameters are explained. In the following section, the SU2 software used for the optimizations is outlined and the optimization method is introduced. Finally, the results of the efficiency optimizations are presented, compared, and analysed.

Druh

D - Stať ve sborníku

CEP obor

IN - Informatika

OECD FORD obor

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Projekt

<a href="/cs/project/LO1303" target="_blank" >LO1303: Podpora udržitelnosti a rozvoje Centra bezpečnostních, informačních a pokročilých technologií (CEBIA-Tech)</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>S - Specificky vyzkum na vysokych skolach

Rok uplatnění

2016

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

MENDEL

ISBN

978-80-214-5365-4

ISSN

1803-3814

e-ISSN

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Počet stran výsledku

8

Strana od-do

79-86

Název nakladatele

Brno University of Technology-VUTIUM Brno

Místo vydání

Brno

Místo konání akce

Brno

Datum konání akce

8. 6. 2016

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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