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Aerodynamics of iced airfoil simulated by RANS code (CROSBI ID 589110)

Prilog sa skupa u zborniku | izvorni znanstveni rad | međunarodna recenzija

Majić, Frane ; Virag, Zdravko Aerodynamics of iced airfoil simulated by RANS code // 7th International Congress of Croatian Society of Mechanics / Virag, Zdravko ; Kozmar, Hrvoje ; Smojver, Ivica (ur.). Zagreb: Studio Hrg, 2012. str. 131-132

Podaci o odgovornosti

Majić, Frane ; Virag, Zdravko

engleski

Aerodynamics of iced airfoil simulated by RANS code

In this work the numerical calculations were performed for two-dimensional flow around NACA23012 airfoil with and without ice accretion. Numerical calculations were performed with RANS (Reynolds Averaged Navier-Stokes) solver for incompressible flow with k-epsilon turbulence model (realizable version) implemented in Fluent software package. The calculated results were compared with experimentally determined data. The stall happens at much smaller angles of attack and also the slope of lift coefficient curve is smaller.

aerofoil; ice accretions; lift coefficient; drag coefficient

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Podaci o prilogu

131-132.

2012.

objavljeno

Podaci o matičnoj publikaciji

7th International Congress of Croatian Society of Mechanics

Virag, Zdravko ; Kozmar, Hrvoje ; Smojver, Ivica

Zagreb: Studio Hrg

9789536986057

Podaci o skupu

7th International Congress of Croatian Society of Mechanics

predavanje

22.05.2012-25.05.2012

Zadar, Hrvatska

Povezanost rada

Strojarstvo, Zrakoplovstvo, raketna i svemirska tehnika