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March 17, 2010, 07:14 |
what is the actual order in a shock region
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#1 |
New Member
mahmoud
Join Date: Mar 2010
Posts: 3
Rep Power: 16 |
Hi
I have a quick question, please I use a second order accurate scheme to solve a problem involving a shock wave (density-based solver). I was told hat in the regions of high gradients (as in the case of shock wave), Fluent switches to a first order scheme, so the final accuarcy will be a first order anyway . Is that true? Thanks |
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March 17, 2010, 10:57 |
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#2 |
Senior Member
Join Date: Nov 2009
Posts: 411
Rep Power: 19 |
Usually a high order scheme (like the one used in Fluent) uses the so called limtator functions near a shock wave - which will actually switch to a first order scheme near a shock wave.
Read any basic CFD book and you will understand exactly why we need to use limiters in these regions. Do |
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March 18, 2010, 04:53 |
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#3 |
New Member
Join Date: Jul 2009
Posts: 7
Rep Power: 16 |
DoHander
is there a reference in Fluent documentation for what you have just said? I've tried to search, but i can't find it... Also i would appreciate if you could suggest some good references that deal with shock wave simulation in CFD... Thanks, muketa |
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March 18, 2010, 08:01 |
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#4 |
Senior Member
Join Date: Nov 2009
Posts: 411
Rep Power: 19 |
For theory - try "Modern compressible flow" by J.D.Anderson
For CFD - "Numerical simulation of internal and external flows" by Hirsch (especially volume II). Here is a better explanation (not written by me) of what I mean: http://www.cfd-online.com/Wiki/Flux_limiters Do |
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