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Forum: FLUENT

December 7, 2015, 08:53

Replies: 3

Finding the stall angle of an airfoil through rotating transient

Views: 1,821

Posted By shereez234

You can manually Enter X and Y component of...

You can manually Enter X and Y component of Velocity in the boundary condition i.e. if Angle of Attack = 0 then X component of Vel = 1 and Y component of Vel = 0 m/s. ( Using cosine relations -...

Forum: FLUENT

December 6, 2015, 15:29

Replies: 3

Finding the stall angle of an airfoil through rotating transient

Views: 1,821

Posted By shereez234

What you are stressing on is a Dynamic Meshing...

What you are stressing on is a Dynamic Meshing Mode which you can achieve through a UDF (User Defined Function).
Stall happens at a certain angle of attack when the Lift force suddenly drops.
You...

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