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Search: Posts Made By: farzadpourfattah
Forum: FLUENT August 28, 2014, 11:04
Replies: 13
Views: 3,690
Posted By farzadpourfattah
CFD Post

Yes you can.
in expression tab you can define Drag coef:
Foorce X@airfoil/0.5*density*Velocity*Velocity*chord length*Span
Forum: FLUENT August 21, 2013, 13:30
Replies: 13
Views: 3,690
Posted By farzadpourfattah
use length of chord airfoil as length scale of...

use length of chord airfoil as length scale of turbulence and intensity 0.1%
Forum: FLUENT March 9, 2013, 15:22
Replies: 13
Views: 3,690
Posted By farzadpourfattah
daer...

if your mach number is:
less than 0.3, chose constant density,
bigger than 0.3 chose ideal gas.(Notice that if you select ideal gas, energy equation tuned on automatically and you should set...
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