Fluent 12.0 --3d airfoil simulation--
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 |
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