[Katloy]

ADAM A500 AIRFOIL

Conditions:
Altitude, ft
0
25000
0
25000

Airspeed, KEAS
220
220
160
160

Ma
0.332588226
0.545965576
0.241882346
0.397065873

AOA,deg
3
3
-1
-1

Yaw angle, deg
0
0
22.5
22.5


I am now doing a 3D simulation of the above airfoil and conditions on Fluent.
It includes compressible and incompressible flow over the wing.
What I don't know is how to set the conditions in the fluent.
As I am a very new comer. I beg your generous help and tips for me to finish the work.
It is urgent as I need to finished it as quick as possible.
I found many youtubes and watched some related pfd. But it is rare to find some useful 3D related works.
So, i post here to ask for any pofessionals help.
THX