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October 31, 2010, 15:18
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Suction
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Senior Member
Morteza
Join Date: May 2010
Location: Iran,Islamic Republic of
Posts: 161
Rep Power: 15  |
hi all...i wrote a code that solves the N-S equations over any airfoil in any speed regimes........i want to add a suction hole in a place or places over the upper side of airfoil in a specific angle and velocity....how can i give the boundary condition for that hole?
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