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Forum: FLUENT

August 7, 2012, 02:25

Replies: 14

Getting lift force at zero angle of attack

Views: 5,925

Posted By hhh

fluent doubt

Dear Shamoon Jamshed,

thanks for your information.

Forum: FLUENT

August 6, 2012, 03:56

Replies: 14

Getting lift force at zero angle of attack

Views: 5,925

Posted By hhh

fluent doubt

Dear Shamoon Jamshed,
thanks for your kind response, i take 2D naca0012 airfoil & and make 3D wing for that i extrude 100mm and meshed in gambit.my boundary conditions are...

Forum: FLUENT

August 3, 2012, 05:44

Replies: 14

Getting lift force at zero angle of attack

Views: 5,925

Posted By hhh

angle of attack

Dear friends,
In fluent, For analysis of 2D naca0012 airfoil velocity inlet we give vcostheta in x component & vsintheta in y component, v is inlet velocity.

1)here i start...

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