Examples
of Data Visualization using Se.La.Vi.
Title : Steady
CFD calculation around airfoil
Flow calculations performed
by : Yannis
Perivolaris
Description :
Steady CFD calculation of airfoil
based
on RANS equations including two-zonal
turbulence model and estimation
of the
transition station.
Calculation conditions :
A.
NACA 0012
angle of attack 12 deg
free transition
Reynolds number 760 000
velocities
B.
GA(W)-1
angle of attack 4 deg
free transition
Reynolds number 6 000 000
velocities
pressure
coefficients
pressure
coefficients and velocities ( trailing edge , after 0.8*c
)
C.
GA(W)-1
angle of attack 16 deg
free transition
Reynolds number 6 000 000
velocities
pressure
coefficients
velocities
( trailing edge , after 0.8*c)
velocities
( reciculation area , trailing edge separation after 0.8*c
)
Back
To Se.La.Vi HOME PAGE
Copyright © 1996 , 1997 N.T.U.A. Fluids Section
For comments , bugs report and information e-mail adress
: aiolos@fluid.mech.ntua.gr
velocities
velocities
pressure
coefficients
pressure
coefficients and velocities ( trailing edge , after 0.8*c
)
velocities
pressure
coefficients
velocities
( trailing edge , after 0.8*c)
velocities
( reciculation area , trailing edge separation after 0.8*c
)