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Forum: FLUENT

March 29, 2012, 04:34

Replies: 27

Airfoil 2D help

Views: 5,137

Posted By Tom Lucius

The chord length which I used in Fluent is by...

The chord length which I used in Fluent is by default (1m).
The published paper's chord length is 15.24 cm and span is 0.91 m.
I not good in using Fluent, so I do not know how to make the chord...

Forum: FLUENT

March 28, 2012, 23:07

Replies: 27

Airfoil 2D help

Views: 5,137

Posted By Tom Lucius

I thought the lift and drag coefficient is...

I thought the lift and drag coefficient is obtained from Fluent. Maybe I am misunderstood the tutorial.

As you mention, after I getting Fluent result (lift & drag coefficient), I must calculate by...

Forum: FLUENT

March 28, 2012, 22:35

Replies: 27

Airfoil 2D help

Views: 5,137

Posted By Tom Lucius

Re = 360,000 Angle of attack = 4 degree ...

Re = 360,000
Angle of attack = 4 degree

Type of Solver = Density Based

Viscous = Inviscid

Boundary Conditions:
Inlet = Velocity inlet
Outlet = Pressure outlet

Forum: FLUENT

March 28, 2012, 21:37

Replies: 27

Airfoil 2D help

Views: 5,137

Posted By Tom Lucius

Hi, i am running 2D flow over NACA 0012...

Hi, i am running 2D flow over NACA 0012 simulation based on this tutorial https://confluence.cornell.edu/display/SIMULATION/ANSYS+WB+-+Airfoil+-+All+Pages.

The default chord length i get is 1 m. ...

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