Aerodynamics of iced airfoil simulated by RANS code (CROSBI ID 589110)
Prilog sa skupa u zborniku | izvorni znanstveni rad | međunarodna recenzija
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