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Forum: STAR-CCM+

January 6, 2010, 00:36

Replies: 5

Airfoil problem

Views: 2,721

Posted By AirWolf

I assume the solution is steady state. what do...

I assume the solution is steady state.
what do u mean by structured or unstructured mesh?
I suspect my mesh is not good enough.
Therefore, I need to redo my work.
What do u think the suitable...

Forum: STAR-CCM+

January 3, 2010, 23:05

Replies: 5

Airfoil problem

Views: 2,721

Posted By AirWolf

Airfoil problem

Greetings people.
I had some problem with my simulation.
FYI, I need to find the drag & lift coefficient for NACA 0063.
The velocity of the wind is 3 m/s while the chord of the airfoil is 0.15m....

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