Examples
of Data Visualization using Se.La.Vi.
Title : Calculation
of the transonic flow around an airfoil
Flow calculations performed
by : Dimitris
Triantos
Description :
Steady state calculation of the
flow around an
airfoil based on Euler equations.
Calculations
have been made with the parallel
implementation
of a 2nd order ( in time and space
) Flux Vector
Spliting sheme.
Calculation conditions :
NACA 0012
angle of attack 1 deg
Mach at infinity 0.85
"C" type grid
Mach
number
pressure
density
velocity
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
Mach
number
pressure
density
velocity