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June 28, 2011, 04:51 |
boundary condition
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#1 |
New Member
ramila.h
Join Date: Dec 2010
Posts: 29
Rep Power: 15 |
Hello,
PLease can you tell me how to set the boundary condition (vartical adiabatic walls) using finite volume method, upwind scheme; I wrote it like this: AAU=(0.5*dYi*(3.*t[NY][i]-4*t[NY-1][i]+t[NY-2][i])); AAL=(0.5*dYi*(-3.*t[0][i]+4*t[1][i]-t[2][i])); but I don't how to set it at zero??????????? |
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