Volume Generation
The final step towards a finished grid is to generate an outer boundary, assign boundary conditions, and generate the volume grid. The outer boundary is really dependent on the geometry and the problem being solved. For example, the outer boundary for a supersonic case can be much closer than for a subsonic case. For illustration, the outer boundary will be 15 body lengths away in all directions. To start, download the file flying_minnow_clean_split_spaced.igs.gz or continue from the last tutorial.
| 1. Read the file
flying_minnow_clean_split_spaced.igs.gz in with gluing and trimming enabled. Select the two points shown and |
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2. Leaving the point created selected, enter 255 (10x25.5) in
the
field. Leave the start and end angles at the default (0 and 90 respectively).
Click
is selected. Leave the
field at 0.0 but change the
to 90.0 and click
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| 3. Select the surface and point shown and go the
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| 4. Select the surfaces shown and the point shown. Change
the (VX,VY,VZ) fields in the Vector application
to (1,0,0). Click |
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| 5. Select the 6 outer boundary points. Go to the
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| 6. In the |
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| 7. Read (sm -grid gridfilename) in the good grid
(the one generated with reconnection on). The group names are not
retained so find the group containing the outer boundary, |
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| 8. Left click somewhere on the prop close to the cutting plane
and zoom. You can see the viscous packing close to the solid surface.
Set the CuttingPlane to Invisible in the global
graphics edit area. At the top of the |
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This completes the grid generation process. The various functions in thepanel can be used for quality evaluation. Practice is the best way to become proficient in grid generation. Good Luck!