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Forum: FLUENT

February 14, 2010, 07:26

Replies: 4

problem with lift curve in airfoil

Views: 1,762

Posted By thanos

You mean to expand my fluid domain in the y and...

You mean to expand my fluid domain in the y and x directions? This is because flow may have gradients of pressure far away from the airfoil, strong enough to change my exact value of Cl in these...

Forum: FLUENT

February 12, 2010, 07:09

Replies: 4

problem with lift curve in airfoil

Views: 1,762

Posted By thanos

Yes but, in the experiment's report the author...

Yes but, in the experiment's report the author doesn't refer to gauge presure, so i guess this should be zero.

Forum: FLUENT

February 11, 2010, 18:38

Replies: 4

problem with lift curve in airfoil

Views: 1,762

Posted By thanos

problem with lift curve in airfoil

Hello,

I tried to make the diagram a.o.a v.s Cl for a NACA 0012 airfoil but i have a problem. Even though i have accurate results for angles of attack between 0 and 13, then for greater angles...

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