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Boundary Condition

Question asked by kannan mahgee on Apr 25, 2008
Latest reply on May 16, 2008 by Bill McEachern

1) How do I set the boundary of the computational domain to velocitygradient =0 and to static pressure at the outlet of the domain?

2) How do I create the boundary wall conditions of and aerofoil?

3) How do I find the skin friction drag of the aerofoil?

Thank You.