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Forum: Main CFD Forum

May 2, 2012, 05:27

Replies: 3

How to determine the separation point on an airfoil???

Views: 2,240

Posted By truffaldino

For flows which are not quasi 2D: the 3D boundary...

For flows which are not quasi 2D: the 3D boundary layer flow the point of separation is not necessarily a point of zero surface stress

For more details see this forum
...

Forum: Main CFD Forum

May 2, 2012, 04:39

Replies: 3

How to determine the separation point on an airfoil???

Views: 2,240

Posted By truffaldino

This is a point where tangential (shear stress)...

This is a point where tangential (shear stress) force vanishes. This is the point where dv_t/dn=0, where v_t is tangential velocity and n is coordinate normal to the surface

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