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Forces on two body-wing in compressible flow. |
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December 12, 2016, 10:09 |
Forces on two body-wing in compressible flow.
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New Member
federico rovere
Join Date: May 2013
Posts: 11
Rep Power: 12 |
Hello!
i'm having some problems with my forces function in controlDict. I need to calculate forces on two different patches, for a 2D compressible flow over an airfoil is correct my add in controlDict? Code:
functions { forces { type forces; functionObjectLibs ( "libforces.so" ); outputControl timeStep; outputInterval 10; patches (airfoil, spoiler); pName p; UName U; rhoName rhoInf; log true; rhoInf 1; CofR (0.4974612746 -0.01671895744 0.125); } } i'm using rhocentralfoam as solver. my output is something like this: Code:
1.000000e+00 ((5.429676e-03 -6.062612e-02 -1.929098e-21) (0.000000e+00 0.000000e+00 0.000000e+00) (0.000000e+00 0.000000e+00 0.000000e+00)) ((2.273480e-02 2.036128e-03 -2.466588e-02) (0.000000e+00 0.000000e+00 0.000000e+00) (0.000000e+00 0.000000e+00 0.000000e+00)) there are just 6 sets...why? |
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