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November 15, 2015, 09:03 |
Entry capasule meshing
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#1 |
New Member
Join Date: Nov 2015
Posts: 6
Rep Power: 11 |
Hi all,
I'm a new CFD user and also new in the forum, so my questions could be a bit obvious for experienced users. I tried to look for the solutions to my doubts on the web but I didn't find them, that's why I decided to create this thread. I'm going to analyse a capsule for atmospheric entry in which I'm interested in the supersonic to subsonic regimes. My idea was to mesh in ICEM and use Fluent as a solver. Does anybody with more experience think it's a good idea to use both software for this purpose? Also, I started a few days meshing in ICEM and till now I don't know how to approach the problem properly. Should I or would be better to split the geometry and block only a quarter of the geometry since it is a revolution object? I did the blocking for the whole geometry and I'm having troubles with the premesh and computing the mesh. In the first case I get an error and in the second the software crashes when it is at 40%. Any advice and tips would be really appreciated. Thanks in advance, Juan |
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November 19, 2015, 12:07 |
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#2 |
New Member
Sarang
Join Date: Oct 2015
Posts: 22
Rep Power: 11 |
First of all I work for CONVERGENT SCIENCE
If you are looking for something like this then I would recommend CONVERGE CFD. https://drive.google.com/file/d/0B7T...ew?usp=sharing https://drive.google.com/file/d/0B7T...ew?usp=sharing |
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Tags |
entry capsule, icem, meshing, subsonic flow, supersonic flow |
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